AUTOMOTIVE VEHICLES - REQUIREMENTS FOR … (Part 3... · 2020. 10. 16. · Automotive Vehicles...

AIS-004 (Part 3) (Rev.1)

I

AUTOMOTIVE INDUSTRY STANDARD

AUTOMOTIVE VEHICLES -

REQUIREMENTS FOR

ELECTROMAGNETIC

COMPATIBILITY

PRINTED BY

THE AUTOMOTIVE RESEARCH ASSOCIATION OF INDIA

P.B. NO. 832, PUNE 411 004

ON BEHALF OF

AUTOMOTIVE INDUSTRY STANDARDS COMMITTEE

UNDER

CENTRAL MOTOR VEHICLE RULES – TECHNICAL STANDING COMMITTEE

SET-UP BY

MINISTRY OF ROAD TRANSPORT & HIGHWAYS

(DEPARTMENT OF ROAD TRANSPORT & HIGHWAYS)

GOVERNMENT OF INDIA

Sept 2020


II

INTRODUCTION

The Government of India felt the need for a permanent agency to expedite the publication

of standards and development of test facilities in parallel when the work on the

preparation of the standards is going on, as the development of improved safety critical

parts can be undertaken only after the publication of the standard and commissioning of

test facilities. To this end, the erstwhile Ministry of Surface Transport (MOST) has

constituted a permanent Automotive Industry Standards Committee (AISC) vide order

No. RT-11028/11/97-MVL dated September 15, 1997. The permanent CMVR Technical

Standing Committee (CTSC) will approve the standards prepared by AISC. After

approval, the Automotive Research Association of India, (ARAI), Pune, being the

Secretariat of the AIS Committee, has published this standard. For better dissemination

of this information ARAI may publish this document on their web site.

To ensure that the electromagnetic radiations emitted by vehicle and by its various

electronic sub-systems do not cause any undue interference with external systems, a

standard on the permissible limits of such radiations, AIS-004 (Part 1) was in force under

CMVR w.e.f. 1st July 2003.

With the advancement of automotive technology electronic content in automotive

vehicles, especially in engine control, braking control is increasing. Hence a need is felt

to formulate requirements of immunity of vehicles and their electronic sub-systems to

external electromagnetic radiations from e.g. Radio / TV / Mobile Transmitters.

Accordingly, immunity test standard AIS-004 (Part 2) “Electromagnetic Radiated

Immunity of Automotive Vehicles – Requirements and Methods of Tests” is prepared by

the panel constituted by AISC.

While preparing this AIS considerable assistance was derived from following

UN R 10 (Rev.2 ) (Amd. 2) (Supp. 2 to 02 series of Amendment, Date of entry into force

12th August, 2004) : Uniform provisions concerning the Approval of Vehicles with

regard to Electromagnetic Compatibility. As this Standard was undergoing revision to

Rev.3 in European Union. Hence the same AISC panel has been entrusted with the task

of formulating new consolidated standard for the requirements of radiated emissions and

immunity for automotive vehicles in line with UN R 10 (Rev.3).

Subsequently, UNR R 10 (Rev. 3) has been further revised to Rev.5 in European Union.

Hence, the same AISC panel has been entrusted with the task of formulating new

revision of AIS-004 (Part 3) in line with UN R 10 (Rev.5) (05 series of amendments –

Date of Entry into force 9th October 2014). Requirements for Emission and Immunity

tests for vehicle and component in normal mode which are present in AIS-004 (Part 3),

are preserved in AIS-004 (Part 3) (Rev.1). New tests added are for vehicles providing

coupling systems for charging the REESS regarding the control of emissions and

immunity from this connection between vehicle and power grid. For vehicles not having

coupling system connecting vehicle to grid for charging the REESS, these additional

tests in charging mode do not apply.

Composition of the Panel and Automotive Industry Standards Committee (AISC)

responsible for preparation and approval of this standard are given in Annex 23 & 24

respectively.


III

CONTENTS

Clause No. Details Page No.

1. Scope 1/149

2. Definitions 1/149

3. Application for approval 4/149

4. Approval 7/149

5. Specifications in configuration other than REESS

charging mode coupled to power grid.

8/149

6. Additional specifications in configuration “REESS

charging mode coupled to power grid”.

14/149

7. Amendment or extension of a vehicle type approval

following ESA addition or substitution.

30/149

8. Conformity of production. 30/149

9. Modification and extension of type approval of a

vehicle or ESA.

31/149

10 Amendments to UN Regulations After the Level

Described.

32/149

List of Annexes

Annex 1A Technical specifications for type approval of a

vehicle, with respect to electromagnetic

compatibility.

43/149

Annex 1B Technical specifications for type approval of an

electric / electronic sub-assembly, with respect to

electromagnetic compatibility.

48/149

Annex 2 Method of measurement of radiated broadband

electromagnetic emissions from vehicles.

50/149

Annex 3 Method of measurement of radiated narrowband

electromagnetic emissions from vehicles.

62/149

Annex 4 Method of testing for immunity of vehicles to

electromagnetic radiation.

65/149

Annex 5 Method of measurement of radiated broadband

electromagnetic emissions from electrical/electronic

sub assemblies.

78/149

Annex 6 Method of measurement of radiated narrowband

electromagnetic emissions from electrical/electronic

sub assemblies.

84/149

Annex 7 Method(s) of testing for immunity of electrical /

electronic sub-assemblies to electromagnetic

radiation.

87/149


IV

Annex 8 Method(s) of testing for immunity to and emission of

transients of electrical/electronic sub-assemblies.

98/149

Annex 9 Method(s) of testing for emission of harmonics

generated on AC power lines from vehicle.

99/149

Annex 10 Method(s) of testing for emission of voltage changes,

voltage fluctuations and flicker on AC power lines

from vehicle.

102/149

Annex 11 Method(s) of testing for emission of radiofrequency

conducted disturbances on AC or DC power lines

from vehicles.

105/149


conducted disturbances on network and

telecommunication access from vehicles.

110/149

Annex 13 Method of testing for immunity of vehicles to

electrical fast transient / burst disturbances conducted

along AC and DC power lines.

116/149

Annex 14 Method of testing for immunity of vehicles to surges

conducted along AC and DC power lines.

119/149

Annex 15 Method(s) of testing for emission of harmonics

generated on AC power lines from an ESA.

123/149

Annex 16 Method(s) of testing for emission of voltage changes,

voltage fluctuations and flicker on AC power lines

from an ESA.

126/149


conducted disturbances on AC or DC power lines

from an ESA.

129/149


conducted disturbances on network and

telecommunication access from an ESA.

133/149

Annex 19 Method of testing for immunity of an ESA to

Electrical Fast Transient / Burst disturbances


136/149

Annex 20 Method of testing for immunity of ESAs to surges


139/149

Annex 21A Guidelines for deciding applicability, worst case

criteria (WCC) and criteria for extension of approval

(CEA) for radiated immunity test.

143/149


V

Annex 21B Guidelines for deciding applicability, worst case

criteria (WCC) and criteria for extension of approval

(CEA) for radiated emission test.

146/149

Annex 22 Composition of AISC Panel 148/149

Annex 23 Composition of AISC 149/149


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Automotive Vehicles –Requirements for Electromagnetic Compatibility

1.0 SCOPE

This standard applies to:

1.1 Vehicles of categories L, M, N and T (Refer IS 14272 for vehicle category

definitions) with regard to electromagnetic compatibility;

1.2 Components and separate technical units intended to be fitted in these

vehicles with the limitation given in paragraph 3.2.1 with regard to

electromagnetic compatibility.

1.3 It covers:

(a) Requirements regarding the immunity to radiated and conducted

disturbances for functions related to direct control of the vehicle, related

to driver, passenger and other road users' protection and related to

disturbances, which would cause confusion to the driver or other road

users, related to vehicle data bus functionality, related to disturbances,

which would affect vehicle statutory data;

(b) Requirements regarding the control of unwanted radiated and conducted

emissions to protect the intended use of electrical or electronic equipment

at own or adjacent vehicles or nearby, and the control of disturbances

from accessories that may be retrofitted to the vehicle.

(c) Additional requirements for vehicles and ESAs providing coupling

systems for charging the REESS regarding the control of emissions and

immunity from this connection between vehicle and power grid.

2.0 DEFINITIONS

For the purposes of this standard:

2.1 "Electromagnetic compatibility" means the ability of a vehicle or

component(s) or separate technical unit(s) to function satisfactorily in its

electromagnetic environment without introducing intolerable

electromagnetic disturbances to anything in that environment.

2.2 "Electromagnetic disturbance" means any electromagnetic phenomenon

which may degrade the performance of a vehicle or component(s) or separate

technical unit(s), or of any other device, unit of equipment or system operated

in vicinity of a vehicle. An electromagnetic disturbance may be

electromagnetic noise, an unwanted signal or a change in the propagation

medium itself.

2.3 "Electromagnetic immunity" means the ability of a vehicle or

component(s) or separate technical unit(s) to operate without degradation of

performance in the presence of (specified) electromagnetic disturbances

which includes wanted radio frequency signals from radio transmitters or


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radiated in-band emissions of industrial-scientific-medical (ISM) apparatus,

internal or external to the vehicle.

2.4 "Electromagnetic environment" means the totality of electromagnetic

phenomena existing at a given location.

2.5 "Broadband emission" means an emission, which has a bandwidth greater

than that of a particular measuring apparatus or receiver (International

Special Committee on Radio Interference (CISPR) 25, second edition).

2.6 "Narrowband emission" means an emission which has a bandwidth less

than that of a particular measuring apparatus or receiver (CISPR 25, second

edition).

2.7 "Electrical / electronic system" means an electrical and / or electronic

device or set of devices together with any associated electrical connections

which form part of a vehicle but which is not intended to be type approved

separately from the vehicle.

2.8 "Electrical / electronic sub-assembly" (ESA) means an electrical and / or

electronic device or set(s) of devices intended to be part of a vehicle, together

with any associated electrical connections and wiring, which performs one or

more specialized functions. An ESA may be approved at the request of a

manufacturer or his authorized representative as either a "component" or a

"separate technical unit (STU)".

2.9 "Vehicle type" in relation to electromagnetic compatibility, means vehicles

which do not differ essentially in such respects as:

2.9.1 The overall size and shape of the engine compartment;

2.9.2 The general arrangement of the electrical and / or electronic components and

the general wiring arrangement;

2.9.3 The primary material of which the body or shell of the vehicle is constructed

(for example, a steel, aluminum or fiberglass body shell). The presence of

panels of different material does not change the vehicle type provided the

primary material of the body is unchanged. However, such variations must be

notified.

2.10 An "ESA type" in relation to electromagnetic compatibility means ESAs,

which do not differ in such essential respects as:

2.10.1 The function performed by the ESA;

2.10.2 The general arrangement of the electrical and / or electronic components, if

applicable.

2.11 "Vehicle wiring harness" means supply voltage, bus system (e.g. CAN),

signal or active antenna cables, which are installed by the vehicle

manufacturer.


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2.12 "Immunity related functions" are:

(a) Functions related to the direct control of the vehicle:

(i) By degradation or change in: e.g. engine, gear, brake, suspension,

active steering, speed limitation devices;

(ii) By affecting drivers position: e.g. seat or steering wheel positioning;

(iii)By affecting driver's visibility: e.g. dipped beam, windscreen wiper.

(b) Functions related to driver, passenger and other road user protection:

(i) e.g. airbag and safety restraint systems.

(c) Functions which when disturbed cause confusion to the driver or other

road users:

(i) Optical disturbances: incorrect operation of e.g. direction indicators,

stop lamps, end outline marker lamps, rear position lamp, light bars

for emergency system, wrong information from warning indicators,

lamps or displays related to functions in subparagraphs (a) or (b)

which might be observed in the direct view of the driver;

(ii) Acoustical disturbances: incorrect operation of e.g. anti-theft alarm,

horn.

(d) Functions related to vehicle data bus functionality:

(i) By blocking data transmission on vehicle data bus-systems, which are

used to transmit data, required to ensure the correct functioning of

other immunity related functions.

(e) Functions which when disturbed affect vehicle statutory data:

e.g. tachograph, odometer.

(f) Functions related to charging mode when coupled to power grid:

(i) For vehicle test: by leading to unexpected vehicle motion;

(ii) For ESA test: by leading to an incorrect charging condition (e.g.

over-current, over-voltage)

2.13 "REESS" means the rechargeable energy storage system that provides

electric energy for electric propulsion of the vehicle.

2.14 “Portable Charger” means portable EV supply equipment for charging,

delivered by the manufacturer along with each vehicle.

2.15 "Coupling system for charging the REESS" means the electrical circuit

installed in the vehicle and portable charger used for charging the REESS.


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2.16 "REESS charging mode coupled to the power grid" means the normal

charging operation mode of the vehicle and / or charging system.

3.0 APPLICATION FOR APPROVAL

3.1 Approval of a Vehicle Type

3.1.1 The application for approval of a vehicle type, with regard to its

electromagnetic compatibility, shall be submitted by the vehicle

manufacturer.

3.1.2 The technical specifications to be submitted at the time of applying for type

approval are as given in Annex 1A.

3.1.3 The vehicle manufacturer shall draw up a schedule describing all relevant

vehicle electrical / electronic systems or ESAs, body styles, variations in

body material, general wiring arrangements, engine variations, and

wheelbase versions. Relevant vehicle electrical / electronic systems or ESAs

are those which may emit significant broadband or narrowband radiation and

/ or those which are involved in immunity related functions of the vehicle

(see paragraph 2.12.) and those which provide coupling systems for charging

the REESS.

3.1.4 A vehicle representative of the type to be approved shall be selected from this

schedule by mutual agreement between the manufacturer and the Test

Agency. The choice of vehicle shall be based on the electrical / electronic

systems offered by the manufacturer. One or more vehicles may be selected

from this schedule if it is considered by mutual agreement between the

manufacturer and the Test Agency that different electrical / electronic

systems are included which are likely to have a significant effect on the

vehicle's electromagnetic compatibility compared with the first

representative vehicle.

While deciding combinations of different makes, elements having radio

interference control equipment (resistive elements, shielded cap etc.) as

specified by vehicle manufacturer shall only be considered for radiated

emission testing. Different makes of elements not contributing to radio

interference control (non-resistive HT coil, Non-resistive HT cable, magneto,

CDI, non-resistive spark plug, non-resistive spark plug cap etc.) shall not be

considered in the combinations to be tested.

3.1.5 The choice of the vehicle(s) in conformity with paragraph 3.1.4 above shall

be limited to vehicle / electrical / electronic system combinations intended for

actual production.

3.1.6 The manufacturer may supplement the application with a report on tests

which have been carried out. Any such data provided may be used by the Test

Agency for the purpose of issuing type-approval.


5/149

3.1.7 If the Test Agency responsible for the type approval test carries out the test

itself, then a vehicle representative of the type to be approved according to

paragraph 3.1.4. shall be provided.

3.1.8 For vehicles of categories M, N, and T, the vehicle manufacturer shall

provide a statement of frequency bands, power levels, antenna positions and

installation provisions for the installation of radio frequency transmitters

(RF-transmitters), even if the vehicle is not equipped with an RF transmitter

at the time of type approval. This should cover all mobile radio services

normally used in vehicles. This information must be made publicly available

following the type approval.

Vehicle manufacturers shall provide evidence that vehicle performance is not

adversely affected by such transmitter installations.

Note: 1) The above need be declared only for recommended fitments of RF

transmitters.

2) These requirements are deemed to have met if vehicle

manufacturer specifies that there is no provision of fitting RF

transmitters on the vehicle.

3.19 Vehicle type approval shall be applied for both REESS and coupling system

for charging the REESS as they are considered as electrical / electronic

systems.

3.2 ESA Type Approval

3.2.1 Applicability of this standard to ESA:


6/149

3.2.2 The application for approval of a type of ESA with regard to its

electromagnetic compatibility shall be submitted by the vehicle manufacturer

or by the manufacturer of the ESA.

3.2.3 The technical specifications to be submitted at the time of applying for type

approval are as given in Annex 1B.

3.2.4 The manufacturer may supplement the application with a report on tests

which have been carried out. Any such data provided may be used by the Test

Agency for the purpose of issuing type-approval.

3.2.5 If the Test Agency responsible for the type approval test carries out the test

itself, then a sample of the ESA system representative of the type to be

approved shall be provided, if necessary, after discussion with the

manufacturer on, e.g., possible variations in the layout, number of

components, number of sensors. If the Test Agency deems it necessary, it

may select a further sample.

3.2.6 The sample(s) must be clearly and indelibly marked with the manufacturer's

trade name or mark and the type designation.

3.2.7 Where applicable, any restrictions on use should be identified. Any such

restrictions should be included in Annex 1B.


7/149

3.2.8 ESA which are brought to the market as spare parts need no type approval if

they are obviously marked as a spare part by an identification number and if

they are identical and from the same manufacturer as the corresponding

original equipment manufacturer (OEM) part for an already type approved

vehicle.

3.2.9 Components sold, as aftermarket equipment and intended for the installation

in motor vehicles need no type approval if they are not related to immunity

related functions (see paragraph 2.12). In this case, a declaration shall be

issued by the manufacturer that the ESA fulfils the requirements of this

standard and in particular the limits defined in paragraphs 5.5, 5.6, 5.7, 5.8

and 5.9.

4.0 APPROVAL

4.1 Type Approval Procedures

4.1.1 Type Approval of a Vehicle

The following alternative procedures for vehicle type approval may be used

at the discretion of the vehicle manufacturer.

4.1.1.1 Approval of a Vehicle Installation

A vehicle installation may be type approved directly by following the

provisions laid down in paragraph 5 of this standard and if applicable

paragraph 6. If this procedure is chosen by a vehicle manufacturer, no

separate testing of electrical / electronic systems or ESA(s) is required.

4.1.1.2 Approval of Vehicle Type by Testing of Individual ESA’s

A vehicle manufacturer may obtain approval for the vehicle by

demonstrating to the Test Agency that all the relevant (See paragraph 3.1.3.

of this standard) electrical / electronic systems or ESAs have been approved

in accordance with this standard and have been installed in accordance with

any conditions attached thereto.

4.1.1.3 A manufacturer may obtain approval according to this standard if the vehicle

has no equipment of the type, which is subject to immunity or emission tests.

Such approvals do not require testing.

4.1.2 Type Approval of an ESA

Type approval may be granted to an ESA to be fitted either to any vehicle

type (component approval) or to a specific vehicle type or types requested by

the ESA manufacturer (separate technical unit approval).

4.1.3 ESAs, which are intentional RF transmitters, which have not received type

approval in conjunction with a vehicle manufacturer, must be supplied with

suitable installation guidelines


8/149

4.2 Granting of Type Approval

4.2.1 Vehicle

4.2.1.1 If the representative vehicle fulfils the requirements of paragraph 5 of this

standard, type approval shall be granted.

4.2.2 ESA

4.2.2.1 If the representative ESA system(s) fulfil(s) the requirements of paragraph 5

and if applicable paragraph 6 of this standard, type approval shall be granted.

5.0 SPECIFICATION IN CONFIGURATIONS OTHER THAN REESS

CHARGING MODE COUPLED TO THE POWER GRID

5.1 General Specifications

5.1.1 A vehicle and its electrical / electronic system(s) or ESA(s) shall be so

designed, constructed and fitted as to enable the vehicle, in normal conditions

of use, to comply with the requirements of this standard.

5.1.1.1 A vehicle shall be tested for radiated emissions and for immunity to radiated

disturbances. No tests for conducted emissions or immunity to conducted

disturbances are required for vehicle type approval.

5.1.1.2 ESA(s) shall be tested for radiated and conducted emissions, for immunity to

radiated and conducted disturbances.

5.1.2 Before testing the Test Agency has to prepare a test plan in conjunction with

the manufacturer, which contains at least mode of operation, stimulated

function(s), monitored function(s), pass / fail criterion (criteria) and intended

emissions.

5.2 Specifications Concerning Broadband Electromagnetic Radiation from

Vehicles

5.2.1 Method of Measurement

The electromagnetic radiation generated by the vehicle representative of its

type shall be measured using the method described in Annex 2. The method

of measurement shall be defined by the vehicle manufacturer in accordance

with the Test Agency.

5.2.2 Vehicle broadband type approval limits

5.2.2.1 If measurements are made using the method described in Annex 2 using a

vehicle-to-antenna spacing of 10.0 ± 0.2 m, the limits shall be 32 dB

microvolts/m in the 30 to 75 MHz frequency band and 32 to 43 dB

microvolts/m in the 75 to 400 MHz frequency band, this limit increasing

logarithmically with frequencies above 75 MHz as shown in Appendix 2. In

the 400 to 1,000 MHz frequency band the limit remains constant at 43 dB

microvolts/m


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microvolts/m.

5.2.2.3 On the vehicle representative of its type, the measured values, expressed

in dB microvolts/m shall be below the type approval limits

5.3 Specifications Concerning Narrowband Electromagnetic Radiation

from Vehicles



type shall be measured using the method described in Annex 3. These shall

be defined by the vehicle manufacturer in accordance with the Test Agency.

5.3.2 Vehicle narrowband type approval limits

5.3.2.1 If measurements are made using the method described in Annex 3 using

a vehicle-to-antenna spacing of 10.0 ± 0.2 m, the limits shall be 22 dB





microvolts/m.

5.3.2.2 If measurements are made using the method described in Annex 3 using

a vehicle-to-antenna spacing of 3.0 ± 0.05 m, the limit shall be 32 dB





microvolts/m

5.3.2.3 On the vehicle representative of its type, the measured values, expressed

in dB microvolts/m, shall be below the type approval limit.

5.3.2.4 Notwithstanding the limits defined in paragraphs 5.3.2.1, 5.3.2.2 and 5.3.2.3

of this standard, if, during the initial step described in paragraph 1.3. of

Annex 3 , the signal strength measured at the vehicle broadcast radio antenna

is less than 20 dB microvolts over the frequency range 76 to 108 MHz

measured with an average detector, then the vehicle shall be deemed to

comply with the limits for narrowband emissions and no further testing will

be required.


10/149

5.4 Specifications Concerning Immunity of Vehicles to Electromagnetic

Radiation.

5.4.1 Method of Testing

The immunity to electromagnetic radiation of the vehicle representative of its

type shall be tested by the method described in Annex 4.

5.4.2 Vehicle Immunity Type Approval Limits.

5.4.2.1 If tests are made using the method described in Annex 4, the field strength

shall be 30 volts/m rms (root mean squared) in over 90 percent of

the 20 to 2,000 MHz frequency band and a minimum of 25 volts/m rms over

the whole 20 to 2,000 MHz frequency band.

5.4.2.2 The vehicle representative of its type shall be considered as complying with

immunity requirements if, during the tests performed in accordance with

Annex 4, there shall be no degradation of performance of "immunity related

functions

5.5 Specifications Concerning Broadband Electromagnetic Interference

Generated by ESAs.


The electromagnetic radiation generated by the ESA representative of its

type shall be measured by the method described in Annex 5.

5.5.2 ESA Broadband Type Approval limits

5.5.2.1 If measurements are made using the method described in Annex 5, the limits

shall be 62 to 52 dB microvolts/m in the 30 to 75 MHz frequency band, this

limit decreasing logarithmically with frequencies above 30 MHz,

and 52 to 63 dB microvolts/m in the 75 to 400 MHz band, this limit

increasing logarithmically with frequencies above 75 MHz as shown in

Appendix 6. In the 400 to 1,000 MHz frequency band the limit remains

constant at 63 dB microvolts/m.

5.5.2.2 On the ESA representative of its type, the measured values, expressed in dB

microvolts/m, shall be below the type approval limits.

5.6 Specifications Concerning Narrowband Electromagnetic Interference

Generated by ESAs.


The electromagnetic radiation generated by the ESA representative of its

type shall be measured by the method described in Annex 6.

5.6.2 ESA narrowband type approval limits


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shall be 52 to 42 dB microvolts/m in the 30 to 75 MHz frequency band, this

limit decreasing logarithmically with frequencies above 30 MHz,

and 42 to 53 dB microvolts/m in the 75 to 400 MHz band, this limit

increasing logarithmically with frequencies above 75 MHz as shown in

Appendix 7. In the 400 to 1,000 MHz frequency band the limit remains

constant at 53 dB microvolts/m.


microvolts/m, shall be below the type approval limits.

5.7 Specifications Concerning Immunity of ESAs to Electromagnetic

Radiation.

5.7.1 Method(s) of Testing

The immunity to electromagnetic radiation of the ESA representative of its

type shall be tested by the method(s) chosen from those described in

Annex 7.

5.7.2 ESA immunity type approval limits

5.7.2.1 If tests are made using the methods described in Annex 7, the immunity test

levels shall be 60 volts/m for the 150 mm stripline testing

method, 15 volts/m for the 800 mm stripline testing method, 75 volts/m for

the Transverse Electromagnetic Mode (TEM) cell testing method, 60 mA for

the bulk current injection (BCI) testing method and 30 volts/m for the free

field testing method in over 90 per cent of the 20 to 2,000 MHz frequency

band, and to a minimum of 50 volts/m for the 150 mm stripline testing

method, 12.5 volts/m for the 800 mm stripline testing method, 62.5 volts/m

for the TEM cell testing method, 50 mA for the bulk current injection (BCI)

testing method and 25 volts/m for the free field testing method over the

whole 20 to 2,000 MHz frequency band.

5.7.2.2 The ESA representative of its type shall be considered as complying with



functions".

5.8 Specifications Concerning the Immunity to Transient Disturbances

Conducted along Supply Lines.

5.8.1 Method of testing

The immunity of ESA representative of its type shall be tested by the

method(s) according to ISO 7637-2, second edition 2004 as described in

Annex 8 with the test levels given in table 1.


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Table 1

Immunity of ESA

Test pulse

number

Immunity

test level Functional status for systems:

Related to

immunity

related

functions

Not related to

immunity

related functions

1 III C D

2a III B D

2b III C D

3a/3b III A D

4 III B

(For ESA

which must be

operational

during engine

start phases)

C

(For other ESA)

D

5.9

Specifications Concerning the Emission of Transient Conducted

Disturbances


The emission of ESA representative of its type shall be tested by the

method(s) according to ISO 7637-2, second edition 2004 as described in

Annex 8 for the levels given in table 2.


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Table 2

Maximum allowed pulse amplitude

Maximum allowed pulse amplitude for

Polarity of pulse

amplitude Vehicles with

12 V systems

Vehicles with

24 V systems

Positive +75 +150

Negative -100 - 450

5.10

Exceptions

5.10.1 Where a vehicle or electrical / electronic system or ESA does not include an

electronic oscillator with an operating frequency greater than 9 kHz, it shall

be deemed to comply with paragraphs 5.3.2 or 5.6.2 above and to

Annexes 3 and 6.

5.10.2 Vehicles which do not have electrical / electronic systems with "immunity

related functions" need not be tested for immunity to radiated disturbances

and shall be deemed to comply with paragraph 5.4 and with Annex 4 to this

standard.

5.10.3 ESAs with no immunity related functions need not be tested for immunity to

radiated disturbances and shall be deemed to comply with paragraph 5.7 and

with Annex 7 to this standard.

5.10.4 Electrostatic Discharge

For vehicles fitted with tyres, the vehicle body / chassis can be considered to

be an electrically isolated structure. Significant electrostatic forces in relation

to the vehicle's external environment occur only at the moment of occupant

entry into or exit from the vehicle. As the vehicle is stationary at these

moments, no type approval test for electrostatic discharge is deemed

necessary.

5.10.5 Conducted Emission

ESAs that are not switched, contain no switches or do not include inductive

loads need not be tested for conducted emission and shall be deemed to

comply with paragraph 5.9.

5.10.6 The loss of function of receivers during the immunity test, when the test

signal is within the receiver bandwidth (RF exclusion band) as specified for

the specific radio service / product in the harmonized international EMC

standard, does not necessarily lead to fail criteria.


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5.10.7 RF transmitters shall be tested in the transmit mode. Wanted emissions

(e.g. from RF transmitting systems) within the necessary bandwidth and out

of band emissions are disregarded for the purpose of this standard. Spurious

emissions are subject to this standard.

5.10.7.1 "Necessary Bandwidth": for a given class of emission, the width of the

frequency band which is just sufficient to ensure the transmission of

information at the rate and with the quality required under specified

conditions (Article 1, No. 1.152 of the ITU Radio Standards).

5.10.7.2 "Out-of-band Emissions": Emission on a frequency or frequencies

immediately outside the necessary bandwidth which results from the

modulation process, but excluding spurious emissions (Article 1, No. 1.144

of the ITU Radio Standards).

5.10.7.3 "Spurious Emission": In every modulation process additional undesired

signals exist. They are summarized under the expression "spurious

emissions". Spurious emissions are emissions on a frequency or frequencies,

which are outside the necessary bandwidth and the level of which may be

reduced without affecting the corresponding transmission of information.

Spurious emissions include harmonic emissions, parasitic emissions,

intermodulation products and frequency conversion products, but exclude

out-of-band emissions (Article 1 No. 1.145 of the ITU Radio Standards)."

6.0 ADDITIONAL SPECIFICATIONS IN THE CONFIGURATION

"REESS CHARGING MODE COUPLED TO THE POWER GRID"

6.1 General specifications

6.1.1 A vehicle and its electrical / electronic system(s) or ESA(s) shall be so

designed, constructed and fitted as to enable the vehicle, in configuration

"REESS charging mode coupled to the power grid", to comply with the

requirements of this standard.

6.1.1.1 A vehicle in configuration "REESS charging mode coupled to the power

grid" shall be tested for radiated emissions, immunity to radiated

disturbances, conducted emissions and immunity to conducted disturbances.

6.1.1.2 ESAs in configuration "REESS charging mode coupled to the power grid"

shall be tested for radiated and conducted emissions, for immunity to radiated

and conducted disturbances

6.1.2 Before testing the Test Agency has to prepare a test plan in conjunction with

the manufacturer, for the configuration "REESS charging mode coupled to

the power grid" configuration which contains at least mode of operation,

stimulated function(s), monitored function(s), pass / fail criterion (criteria)

and intended emissions.


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6.1.3 A vehicle in configuration "REESS charging mode coupled to the power

grid" should be tested with the charging cable delivered by the manufacturer.

In this case, the cable shall be type approved as part of the vehicle.

6.1.4 Artificial networks

AC Power mains shall be applied to the vehicle / ESA through

50 μH / 50-AN(s) as defined in CISPR 16-1-2 paragraph 4.3.

DC Power mains shall be applied to the vehicle / ESA through

5 μH / 50 - AN(s) as defined in CISPR 25.

High voltage power line shall be applied to the ESA through a

5 μH / 50 -HV-AN(s) as defined in Appendix 8. E/ECE/324/Add.9/Rev.5

E/ECE/TRANS/505/Add.9/Rev.5

6.2 Specifications concerning broadband electromagnetic radiation from

vehicles

6.2.1 Method of measurement


type shall be measured using the method described in Annex 2. The method

of measurement shall be defined by the vehicle manufacturer in accordance


6.2.2. Vehicle broadband type approval limits







microvolts/m.







microvolts/m.

On the vehicle representative of its type, the measured values, expressed in

dB microvolts/m shall be below the type approval limits.

6.3 Specifications concerning emission of harmonics on AC power lines

from vehicles


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The harmonics emission on AC power lines generated by the vehicle

representative of its type shall be measured using the method described in

Annex 9. The method of measurement shall be defined by the vehicle

manufacturer in accordance with the Test Agency.

6.3.2 Vehicle type approval limit


for input current ≤ 16 A per phase are those defined in IEC 61000-3-2 and

given in Table 3.

Table 3

Maximum allowed harmonics (input current ≤ 16 A per phase)

Harmonic number (n) Maximum authorized harmonic current A

Odd harmonics

3 2.3

5 1.14

7 0.77

9 0.40

11 0.33

13 0.21

15 ≤ n ≤ 39 0.15x15/n

Even harmonics

2 1.08

4 0.43

6 0.30

8 ≤ n ≤ 40 0.23x8/n

6.3.2.2

If measurements are made using the method described in Annex 9, the limits

for input current > 16 A and ≤ 75 A per phase are those defined in IEC

61000-3-12, and given in given in Table 4, Table 5 and Table 6.


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Table 4

Maximum allowed harmonics (input current > 16 A and ≤ 75 A per

phase) for equipment other than balanced three-phase equipment

Minimum

Rsce

Acceptable individual harmonic

current In/I1 %

Maximum current

harmonic ratio %

I3 I5 I7 I9 I11 I13 THD PWHD

33 21.6 10.7 7.2 3.8 3.1 2 23 23

66 24 13 8 5 4 3 26 26

120 27 15 10 6 5 4 30 30

250 35 20 13 9 8 6 40 40

≥ 350 41 24 15 12 10 8 47 47

Relative values of even harmonics lower or equal to 12 shall be lower than

16/n %. Even harmonics greater than 12 are taken into account in the Total

Harmonic Distortion (THD) and Partial Weighted Harmonic Distortion

(PWHD) the same way than odd harmonics.

Linear interpolation between successive values of Short Circuit Ratio of an

Equipment (Rsce) is authorized.

Table 5


phase) for balanced three-phase equipment

Minimum

Rsce


current In/I1 %

Maximum current

harmonic ratio %

I5 I7 I11 I13 THD PWHD

33 10.7 7.2 3.1 2 13 22

66 14 9 5 3 16 25

120 19 12 7 4 22 28

250 31 20 12 7 37 38

≥ 350 40 25 15 10 48 46


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16/n %. Even harmonics greater than 12 are taken into account in the THD

and PWHD the same way than odd harmonics.

Linear interpolation between successive values of Rsce is authorized.

Table 6


phase) for balanced three-phase equipment under specific conditions

Minimum

Rsce


current In/I1 %

Maximum

current harmonic

ratio %


33 10.7 7.2 3.1 2 13 22

≥ 120 40 25 15 10 48 46



and PWHD the same way than odd harmonics

6.4 Specifications concerning emission of voltage changes, voltage

fluctuations and flicker on AC power lines from vehicles.


The emission of voltage changes, voltage fluctuations and flicker on AC

power lines generated by the vehicle representative of its type shall be

measured using the method described in Annex 10. The method of

measurement shall be defined by the vehicle manufacturer in accordance


6.4.2. Vehicle type approval limit


for rated current ≤ 16 A per phase and not subjected to conditional connection

are those defined in IEC 61000-3-3, paragraph 5.


for rated current > 16 A and ≤ 75 A per phase and subjected to conditional

connection are those defined in IEC 61000-3-11, paragraph 5.

6.5 Specifications concerning emission of radiofrequency conducted

disturbances on AC or DC power lines from vehicles


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The emission of radiofrequency conducted disturbances on AC or DC power

lines generated by the vehicle representative of its type shall be measured

using the method described in Annex 11. The method of measurement shall

be defined by the vehicle manufacturer in accordance with the Test Agency.



on AC power lines are those defined in IEC 61000-6-3 and given in Table 7.

Table 7

Maximum allowed radio frequency conducted disturbances on

AC power lines

Frequency (MHz) Limits and detector

0.15 to 0.5 66 to 56 dBμV (quasi-peak) 56 to 46 dBμV (average)

(Linearly decreasing with logarithm of frequency)

0.5 to 5 56 dBμV (quasi-peak) 46 dBμV (average)

5 to 30 60 dBμV (quasi-peak) 50 dBμV (average)


on DC power lines are those defined in IEC 61000-6-3 and given in Table 8.

Table 8

Maximum allowed radiofrequency conducted disturbances on DC

power lines


0.15 to 0.5 79 dBμV (quasi-peak)

66 dBμV (average)

0.5 to 30 73 dBμV (quasi-peak)

60 dBμV (average)


disturbances on network and telecommunication access from vehicles


The emission of radiofrequency conducted disturbances on network and

telecommunication access generated by the vehicle representative of its type

shall be measured using the method described in Annex 12. The method of


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measurement shall be defined by the vehicle manufacturer in accordance




on network and telecommunication access (telecommunication access as

defined in paragraph 3.1.32 of CISPR 32) are those defined in IEC 61000-6-3

and given in Table 9.

Table 9

Maximum allowed radiofrequency conducted disturbances on network

and telecommunication access

Frequency (MHz) Voltage limits (detector) Current limits

(detector)

0.15 to 0.5 84 to 74 dBμV (quasi-peak) 40 to 30 dBμA

(quasi-peak)

74 to 64 dBμV (average)

(linearly decreasing with

logarithm of frequency)

30 to 20 dBμA (average)



0.5 to 30 74 dBμV (quasi-peak) 30 dBμA (quasi-peak)

64 dBμV (average) 20 dBμA (average)

6.7

Specifications concerning immunity of vehicles to electromagnetic

radiation


The immunity to electromagnetic radiation of the vehicle representative of its

type shall be tested by the method described in Annex 4.

6.7.2 Vehicle immunity type approval limits

6.7.2.1 If tests are made using the method described in Annex 4, the field strength

shall be 30 volts/m rms (root mean squared) in over 90 per cent of the 20 to

2,000 MHz frequency band and a minimum of 25 volts/m rms over the whole

20 to 2,000 MHz frequency band.




functions", according to paragraph 2.2. of Annex 4.


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6.8 Specifications concerning the immunity of vehicles to Electrical Fast

Transient / Burst disturbances conducted along AC and DC power lines.


6.8.1.1 The immunity to Electrical Fast Transient / Burst disturbances conducted

along AC and DC power lines of the vehicle representative of its type shall be

tested by the method described in Annex 13.



levels, for AC or DC power lines, shall be: ±2 kV test voltage in open circuit,

with a rise time (Tr) of 5 ns, and a hold time (Th) of 50 ns and a repetition rate

of 5 kHz for at least 1 minute.





6.9 Specifications concerning the immunity of vehicles to surge conducted

along AC or DC power lines.


6.9.1.1 The immunity to surge conducted along AC / DC power lines of the vehicle

representative of its type shall be tested by the method described in

Annex 14.



levels shall be:

(a) For AC power lines: ±2 kV test voltage in open circuit between line and

earth and ±1 kV between lines (pulse 1.2 μs / 50 μs), with a rise time (Tr)

of 1.2 μs, and a hold time (Th) of 50 μs. Each surge shall be applied five

times with a maximum delay of 1 minute between each pulse. This has to

be applied for the following phases: 0, 90, 180 and 270°,

(b) For DC power lines: ±0.5 kV test voltage in open circuit between line and

earth and ±0.5 kV between lines (pulse 1.2 μs / 50 μs) with a rise time (Tr)


times with a maximum delay of 1 minute.





6.10 Specifications concerning broadband electromagnetic interference

caused by ESAs


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The electromagnetic radiation generated by the ESA representative of its type

shall be measured by the method described in Annex 5.

6.10.2 ESA broadband type approval limits


shall be 62 to 52 dB μV/m in the 30 to 75 MHz frequency band, this limit

decreasing logarithmically with frequencies above 30 MHz, and 52 to 63 dB

μV/m in the 75 to 400 MHz band, this limit increasing logarithmically with

frequencies above 75 MHz as shown in Appendix 6. In the 400 to 1,000 MHz

frequency band the limit remains constant at 63 dB μV/m.


μV/m, shall be below the type approval limits.

6.11 Specifications concerning emission of harmonics on AC power lines from

ESAs


The harmonics emission on AC power lines generated by the ESA representative

of its type shall be measured using the method described in Annex 15. The

method of measurement shall be defined by the manufacturer in accordance with

the Test Agency.

6.11.2 ESA type approval limit

6.11.2.1


for input current ≤ 16 A per phase are those defined in IEC 61000-3-2 and given

in Table 10.

Table 10

Maximum allowed harmonics (input current ≤ 16 A per phase)

Harmonic number, n Maximum authorized harmonic

current, A

Odd harmonics

3 2.3

5 1.14

7 0.77

9 0.40

11 0.33

13 0.21

15 ≤ n ≤ 39 0.15x15/n

Even harmonics

2 1.08

4 0.43

6 0.30

8 ≤ n ≤ 40 0.23x8/n

6.11.2.2. If measurements are made using the method described in Annex 15, the

limits for input current > 16 A and ≤ 75 A per phase are those defined in IEC

61000-3-12 and given in Table 11, Table 12 and Table 13.


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Table 11


phase) for equipment other than balanced three-phase equipment.

Minimum

Rsce


current In/I1 %

Maximum current

harmonic ratio %

I3 I5 I7 I9 I11 I13 THD PWHD

33 21.

6

10.

7

7.2 3.8 3.1 2 23 23

66 24 13 8 5 4 3 26 26

120 27 15 10 6 5 4 30 30

250 35 20 13 9 8 6 40 40

≥ 350 41 24 15 12 10 8 47 47



and PWHD in the same way than odd harmonics.


Table 12


phase) for balanced three-phase equipment.

Minimum

Rsce


current In/I1 %

Maximum current

harmonic ratio %


33 10.7 7.2 3.1 2 13 22

66 14 9 5 3 16 25

120 19 12 7 4 22 28

250 31 20 12 7 37 38

≥ 350 40 25 15 10 48 46


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and PWHD in the same way as odd harmonics.


Table 13


phase) for balanced three-phase equipment under specific conditions

Minimum

Rsce


current In/I1 %

Maximum current

harmonic ratio %


33 10.7 7.2 3.1 2 13 22

≥ 120 40 25 15 10 48 46



and PWHD in the same way as odd harmonics.

6.12 Specifications concerning emission of voltage changes, voltage

fluctuations and flicker on AC power lines from ESAs


The emission of voltage changes, voltage fluctuations and flicker on AC

power lines generated by the ESA representative of its type shall be

measured using the method described in Annex 16. The method of

measurement shall be defined by the ESA manufacturer in accordance with

the Test Agency.


6.12.2.1 If measurements are made using the method described in Annex 16, the

limits for rated current ≤ 16 A per phase and not subjected to conditional

connection are those defined in IEC 61000-3-3, paragraph 5.


limits for rated current > 16 A and ≤ 75 A per phase and subjected to

conditional connection are those defined in IEC 61000-3-11, paragraph 5.


disturbances on AC or DC power lines from ESA


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The emission of radiofrequency conducted disturbances on AC or DC power

lines generated by the ESA representative of its type shall be measured

using the method described in Annex 17. The method of measurement shall

be defined by the ESA manufacturer in accordance with the Test Agency.



limits on AC power lines are those defined in IEC 61000-6-3 and given in

Table 14.

Table 14

Maximum allowed radiofrequency conducted disturbances on AC power

Lines Frequency

(MHz)

Limits and detector

0.15 to 0.5 66 to 56 dBμV (quasi-peak) 56 to 46 dBμV

(average)

(linearly decreasing with logarithm of frequency)


5 to 30 60 dBμV (quasi-peak) 50 dBμV (average)


on DC power lines are those defined in IEC 61000-6-3 and given in Table 15.

Table 15

Maximum allowed radiofrequency conducted disturbances on DC power

lines


0.15 to 0.5 79 dBμV (quasi-peak) 66 dBμV (average)


6.14

Specifications concerning emission of radiofrequency conducted

disturbances on network and telecommunication access from ESA


The emission of radiofrequency conducted disturbances on network and

telecommunication access generated by the ESA representative of its type shall

be measured using the method described in Annex 18. The method of

measurement shall be defined by the ESA manufacturer in accordance with the

Test Agency.


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limits on network and telecommunication access (telecommunication access

as defined in paragraph 3.1.32 of CISPR 32) are those defined in IEC

61000-6-3 and given in Table 16.

Table 16

Maximum allowed radiofrequency conducted disturbances on network

and telecommunication access

Frequency (MHz) Voltage limits (detector) Current limits

(detector)

0.15 to 0.5 84 to 74 dBμV (quasi-peak)

74 to 64 dBμV (average)



40 to 30 dBμA

(quasi-peak) 30 to 20

dBμA (average)

(linearly decreasing

with logarithm of

frequency)

0.5 to 30 74 dBμV (quasi-peak) 64

dBμV (average)

30 dBμA (quasi-peak)

20 dBμA (average)

6.15 Specifications concerning the immunity of ESAs to electrical fast

transient/burst disturbances conducted along AC and DC power lines.


6.15.1.1 The immunity to Electrical Fast Transient / Burst disturbances conducted

along AC and DC power lines of the ESA representative of its type shall be

tested by the method described in Annex 19.


6.15.2.1 If tests are made using the methods described in Annex 19, the immunity

test levels, for AC or DC power lines, shall be: ± 2 kV test voltage in open

circuit, with a rise time (Tr) of 5 ns, and a hold time (Th) of 50 ns and a

repetition rate of 5 kHz for at least 1 minute.



Annex19, there shall be no degradation of performance of "immunity related


6.16 Specifications concerning the immunity of ESAs to surge conducted

along AC or DC power lines



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6.16.1.1 The immunity to surge conducted along AC / DC power lines of the ESA

representative of its type shall be tested by the method described in

Annex 20.


6.16.2.1 If tests are made using the methods described in Annex 20, the immunity

test levels shall be:

(a) For AC power lines: ±2 kV test voltage in open circuit between line and

earth and ±1 kV between lines (pulse 1.2 μs / 50 μs), with a rise time (Tr)


times with a maximum delay of 1 minute between each pulse. This has to

be applied for the following phases: 0, 90, 180 and 270°,

(b) For DC power lines: ±0.5 kV test voltage in open circuit between line

and earth and ±0.5 kV between lines (pulse 1.2 μs / 50 μs) with a rise

time (Tr) of 1.2 μs, and a hold time (Th) of 50 μs. Each surge shall be

applied five times with a maximum delay of 1 minute.



Annex 20, there shall be no degradation of performance of "immunity

related functions", according to paragraph 2.2. of Annex 7.

6.17 Specifications concerning the emission of transient conducted

disturbances generated by ESAs on 12 / 24 V supply lines


The emission of ESA representative of its type shall be tested by the

method(s) according to ISO 7637-2, as described in Annex 8 for the levels

given in Table 17.

Table 17

Maximum allowed pulse amplitude

Maximum allowed pulse amplitude for

Polarity of pulse amplitude Vehicles with 12 V

systems

Vehicles with 24V

systems

Positive +75 V +150 V

Negative –100 V –450 V


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6.18 Specifications concerning immunity of ESAs to electromagnetic

radiation

6.18.1 Method(s) of testing

The immunity to electromagnetic radiation of the ESA representative of its

type shall be tested by the method(s) chosen from those described in Annex

7.



levels shall be 60 volts/m rms for the 150 mm stripline testing method, 15

volts/m rms for the 800 mm stripline testing method, 75 volts/m rms for the

Transverse Electromagnetic Mode (TEM) cell testing method, 60 mA rms

for the Bulk Current Injection (BCI) testing method and 30 volts/m rms for

the free field testing method in over 90 per cent of the 20 to 2,000 MHz

frequency band, and to a minimum of 50 volts/m rms for the 150 mm

stripline testing method, 12.5 volts/m rms for the 800 mm stripline testing

method, 62.5 volts/m rms, for the TEM cell testing method, 50 mA rms for

the bulk current injection (BCI) testing method and 25 volts/m rms for the

free field testing method over the whole 20 to 2,000 MHz frequency band.




functions".

6.19 Specifications concerning the immunity of ESAs to transient

disturbances conducted along 12 / 24 V supply lines.


The immunity of ESA representative of its type shall be tested by the

method(s) according to ISO 7637-2, as described in Annex 8 with the test

levels given in Table 18.


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Table 18

Immunity of ESA

Test pulse

number

Immunity

test level

Functional status for systems:

Related to

immunity related

functions

Not related to

immunity

related

functions

1 III C D

2a III B D

2b III C D

3a/3b III A D

4 III B (for ESA which

shall be operational

during engine start

phases)

C (for other ESA)

D

6.20

Exceptions

6.20.1 When there is no direct connection to a telecommunication network which

includes telecommunication service additional to the charging

communication service, Annex 12 and Annex 18 shall not apply.

6.20.2 When network and telecommunication access of the vehicle uses power line

Transmission (PLT) on its AC/DC power lines, Annex 12 shall not apply.

6.20.3 When network and telecommunication access of the ESA uses Power Line

Transmission (PLT) on its AC/DC power lines, Annex 18 shall not apply.

6.20.4 Vehicles and / or ESA which are intended to be used in "REESS charging

mode coupled to the power grid" in the configuration connected to a

DC-charging station with a length of a DC network cable shorter than 30 m

do not have to fulfil the requirements of Annex 11, Annex 13, Annex 14,

Annex 17, Annex 19 and Annex 20.

In this case, the manufacturer shall provide a statement that the vehicle

and/or ESA can be used in "REESS charging mode coupled to the power

grid" only with cables shorter than 30 m. This information shall be made

publicly available following the type approval.


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6.20.5 Vehicles and / or ESA which are intended to be used in "REESS charging

mode coupled to the power grid" in the configuration connected to a local /

private DC-charging station without additional participants do not have to

fulfil requirements of Annexes 11, 13, 14, 17, 19 and 20.

In this case, the manufacturer shall provide a statement that the vehicle and /

or ESA can be used in "REESS charging mode coupled to the power grid"

only with a local/private DC charging station without additional

participants. This information shall be made publicly available following the

type approval.

7.0 AMENDMENT OR EXTENSION OF A VEHICLE TYPE

APPROVAL FOLLOWING ESA ADDITION OR SUBSTITUTION

7.1 Where a vehicle manufacturer has obtained type approval for a vehicle

installation and wishes to fit an additional or substitutional electrical /

electronic system or ESA which has already received approval under this

standard, and which will be installed in accordance with any conditions

attached thereto, the vehicle approval may be extended without further

testing. The additional or substitutional electrical / electronic system or

ESA shall be considered as part of the vehicle for conformity of production

purposes.

7.2 Where the additional or substitutional part(s) has (have) not received

approval pursuant to this standard, and if testing is considered necessary, the

whole vehicle shall be deemed to conform if the new or revised part(s) can

be shown to conform to the relevant requirements of paragraph 5 or if, in a

comparative test, the new part can be shown not to be likely to adversely

affect the conformity of the vehicle type.

7.3 The addition by a vehicle manufacturer to an approved vehicle of standard

domestic or business equipment, other than mobile communication

equipment, which conforms to other standards, and the installation,

substitution or removal of which is according to the recommendations of the

equipment and vehicle manufacturers, shall not invalidate the vehicle

approval. This shall not preclude vehicle manufacturers fitting

communication equipment in accordance with suitable installation

guidelines developed by the vehicle manufacturer and / or manufacturer(s)

of such communication equipment. The vehicle manufacturer shall provide

evidence (if requested by the Test Agency) that vehicle performance is not

adversely affected by such transmitters. This can be a statement that the

power levels and installation are such that the immunity levels of this

standard offer sufficient protection when subject to transmission alone i.e.

excluding transmission in conjunction with the tests specified in

paragraph 5. This standard does not authorize the use of a communication

transmitter when other requirements on such equipment or its use apply.

8.0 CONFORMITY OF PRODUCTION

8.1 Conformity of Production Procedures of a Vehicle fitted with ESA


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8.1.1 A vehicle approved under this standard shall be so manufactured as to

conform to the type approved by meeting the relevant requirements set forth

in this standard.

8.1.2 Whole vehicle conformity of production procedures shall be applicable as

and when notified by the Government (Ministry of Road Transport &

Highways).

8.2 Conformity of Production Procedures of an ESA

8.2.1 ESA approved under this standard shall be so manufactured as to conform to

the type approved by meeting the relevant requirements set forth in this

standard.

8.2.2 Conformity of production procedures as and when notified by the

Government (Ministry of Road Transport & Highways) shall be applicable

9.0 MODIFICATION AND EXTENSION OF TYPE APPROVAL OF

A VEHICLE OR ESA

9.1 Every modification pertaining to the information, even if the changes are not

technical in nature declared in accordance with 3.0, shall be intimated by the

manufacturer to the Test Agency.

If the changes are in parameters not related to the provisions, no further

action will be taken.

If the changes are in parameters related to the provisions, the testing agency

which has issued the certificate of compliance shall then consider whether

9.1.1 The model with the changed specifications still complies with provisions or

9.1.2 Any further verification or testing is required to establish compliance.

9.2 For considering whether testing is required or not, guidelines given in

Annex 21A & 22B (Worst Case Criteria (WCC) & Criteria for Extension of

Approval) shall be used.

9.3 In case of 9.1.2, tests for only those parameters which are affected by the

modifications need to be carried out.

9.4 In case of fulfillment of criterion of para 9.1.1, or after results of further

verification as per para 9.1.2 are satisfactory, the approval of compliance

shall be extended for the changes carried out.


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10.0 AMENDMENTS TO ECE REGULATIONS AFTER THE LEVEL

DESCRIBED

10.1 Supplements

In case of changes in ECE regulation, which are issued as supplements

(Supplements do not affect the earlier type approvals) at the request of

applicant, approval of compliance to this standard shall be issued taking into

account the changes arising out of such supplement(s) to ECE regulation

with approval from Chairman AISC.

This shall be incorporated in the test report.

Note: Such changes will be considered for inclusion in this standard at the

time of its next amendment /revision.

10.2 Series of amendments

Changes in ECE regulation, which are issued as series of amendments

(series of amendments may affect the earlier type approvals) will not be

considered for issuing approval to this standard. However, Chairman, AISC

may, on a case to case basis, permit to accept latest series of amendments.

This shall be incorporated in the test report.

Note: Such changes will be considered for inclusion in this standard at the

time of its next revision.


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APPENDIX 1

LIST OF STANDARDS REFERRED TO IN THIS STANDARD

1.0 CISPR 12 "Vehicles', motorboats' and spark-ignited engine-driven devices'

radio disturbance characteristics - Limits and methods of measurement",

fifth edition 2001.

2.0 CISPR 16-1-4 "Specifications for radio disturbance and immunity measuring

apparatus and methods - Part 1: Radio disturbance and immunity measuring

apparatus", Edition 1.1. 2004.

3.0 CISPR 25 "Limits and methods of measurement of radio disturbance

characteristics for the protection of receivers used on board vehicles",

second edition 2002.

4.0 ISO 7637-1 "Road vehicles - Electrical disturbance from conduction and

coupling - Part 1: Definitions and general considerations", second edition 2002.

5.0 ISO 7637-2 "Road vehicles - Electrical disturbance from conduction and

coupling - Part 2: Electrical transient conduction along supply lines only on

vehicles with nominal 12 V or 24 V supply voltage", second edition 2004.

6.0 ISO EN 17025"General requirements for the competence of testing and

calibration laboratories", second edition 2005 and Corrigendum:2006. Third

Edition 2017

7.0 ISO 11451 "Road vehicles - Electrical disturbances by narrowband radiated

electromagnetic energy - Vehicle test methods":

Part 1: General and definitions (ISO 11451-1, third edition 2005);

Part 2: Off-vehicle radiation source (ISO 11451-2, third edition 2005);

Part 4: Bulk current injection (BCI) (ISO 11451-4, first edition 1995).

8.0 ISO 11452 "Road vehicles - Electrical disturbances by narrowband radiated

electromagnetic energy - Component test methods":

Part 1: General and definitions (ISO 11452-1, third edition 2005);

Part 2: Absorber-lined chamber (ISO 11452-2, second edition 2004);

Part 3: Transverse electromagnetic mode (TEM) cell (ISO 11452-3,

third edition 2001);

Part 4: Bulk current injection (BCI) (ISO 11452-4, third edition 2005);

Part 5: Stripline (ISO 11452-5, second edition 2002).

9.0 ITU Radio Standards, edition 2001.


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10 IEC 61000-3-2 "Electromagnetic Compatibility (EMC) - Part 3-2 - Limits for

harmonic current emissions (equipment input current ≤ 16 A per phase)", edition

3.2 - 2005 + A1: 2008 + A2: 2009

11 IEC 61000-3-3 "Electromagnetic Compatibility (EMC) - Part 3-3 - Limits -

Limitation of voltage changes, voltage fluctuations and flicker in public

low-voltage systems for equipment with rated current ≤ 16 A per phase and not

subjected to conditional connection", edition 2.0 - 2008.

12 IEC 61000-3-11 "Electromagnetic Compatibility (EMC) - Part 3-11 - Limits -

Limitation of voltage changes, voltage fluctuations and flicker in public

low-voltage systems - Equipment with rated current ≤ 75 A per phase and

subjected to conditional connection", edition 1.0 - 2000.

13 IEC 61000-3-12 "Electromagnetic Compatibility (EMC) - Part 3-12 – Limits for

harmonic current emissions produced by equipment connected to public

low-voltage systems with input current > 16 A and ≤ 75 A per phase", edition

1.0 - 2004.

14 IEC 61000-4-4 "Electromagnetic Compatibility (EMC) - Part 4-4 - Testing and

measurement techniques - Electrical fast transient’s/burst immunity test",

edition 2.0 - 2004.

15 IEC 61000-4-5 "Electromagnetic Compatibility (EMC) - Part 4-5 - Testing and

measurement techniques - Surge immunity test", edition 2.0 – 2005.

16 IEC 61000-6-2 "Electromagnetic Compatibility (EMC) - Part 6-2 - Generic

Standards Immunity for industrial environments", edition 2.0 - 2005.

17 IEC 61000-6-3 "Electromagnetic Compatibility (EMC) - Part 6-3 - Generic

Standards Emission standard for residential, commercial and light-industrial

environments", edition 2.0 - 2006.

18 CISPR 16–2–1 "Specification for radio disturbances and immunity measuring

apparatus and methods - Part 2-1 - Methods of measurement of disturbances and

immunity - Conducted disturbances measurement", edition 2.0 - 2008.

19 CISPR 32 "Information Technology Equipment - Radio disturbances

characteristics - Limits and methods of measurement", edition 2.0 - 2015.

20 CISPR 16-1-2 "Specification for radio disturbance and immunity measuring

apparatus and methods - Part 1-2: Radio disturbance and immunity measuring

apparatus - Ancillary equipment - Conducted disturbances", edition 1.2: 2006.

35/149

APPENDIX 2 AIS

-004 (P

art 3

) (Rev

.1)

VEHICLE BROADBAND REFERENCE LIMITS

Antenna-Vehicle Separation: 10 m

Limit E (dBµV/m) at frequency F (MHz)

30 - 75 MHz 75 - 400 MHz 400 – 1,000 MHz

E = 32 E = 32 + 15.13 log (F/75) E = 43

Frequency – megahertz – logarithmic (See paragraph 5.2.2.1 of this standard)

0

10

20

30

40

50

60

10 100 1,000

F (MHz)

E (

dB

µV

/m)

Vehicle radiated emission limit

Broadband type approval limit - 10 m

Quasi-peak detector - 120 kHz bandwidth

36/149

APPENDIX 3

VEHICLE BROADBAND REFERENCE LIMITS

AIS

-004 (P

art 3

) (Rev

.1)



30 - 75 MHz 75 - 400 MHz 400 – 1,000 MHz

E = 42 E = 42 + 15.13 log (F/75) E = 53

Frequency – megahertz - logarithmic

(See paragraph 5.2.2.2 of this standard)

0

10

20

30

40

50

60

10 100 1,000

F (MHz)

E (

dB

µV

/m)


Broadband type approval limit - 3 m Quasi-peak detector - 120 kHz bandwidth

37/149

APPENDIX 4

AIS

-004 (P

art 3

) (Rev

.1)

VEHICLE NARROWBAND REFERENCE LIMITS



30 - 75 MHz 75 - 400 MHz 400 – 1,000 MHz

E = 22 E = 22 + 15.13 log (F/75) E = 33



0

10

20

30

40

50

60

10 100 1000 F (MHz)

E (

dB

µV

/m)


Narrowband type approval limit - 10 m

Average detector - 120 kHz bandwidth

38/149

APPENDIX 5

VEHICLE NARROWBAND REFERENCE LIMITS

AIS

-004 (P

art 3

) (Rev

.1)



30 - 75 MHz 75 - 400 MHz 400 – 1,000 MHz

E = 32 E = 32 + 15.13 log (F/75) E = 43



0

10

20

30

40

50

60

10 100 1000

F (MHz)

E (

dB

µV

/m)




39/149

APPENDIX 6

AIS

-004 (P

art 3

) (Rev

.1)

ELECTRICAL/ELECTRONIC SUB-ASSEMBLY

Broadband Reference Limits


30 - 75 MHz 75 - 400 MHz 400 – 1,000 MHz

E = 62 – 25.13 log (F/30) E = 52 + 15.13 log (F/75) E = 63



20

30

40

50

60

70

10 100 1000

F (MHz)

E (

dB

µV

/m)

ESA radiated emission limit

Broadband type approval limit - 1 m

Quasi-peak detector - 120 kHz bandwidth

40/149

APPENDIX 7

AIS

-004 (P

art 3

) (Rev

.1)

ELECTRICAL/ELECTRONIC SUB-ASSEMBLY

Narrow band Reference Limits


30 - 75 MHz 75 - 400 MHz 400 – 1,000 MHz

E = 52 – 25.13 log (F/30) E = 42 + 15.13 log (F/75) E = 53



20

30

40

50

60

70

10 100 1000

F (MHz)

E (

dB

µV

/m)

ESA radiated emission limit




41/149

APPENDIX 8

HV ARTIFICIAL NETWORK

Figure 1

HV artificial network

Legend C2: 0.1 μF

L1: 5 μH R1: 1 kΩ

C1: 0.1 μF R2: 1 MΩ (discharging C2 to < 50 Vdc within 60 s)

Figure 2

Impedance of HV artificial network


42/149

Figure 3

Combination of HV artificial network


43/149

ANNEX 1A

TECHNICAL SPECIFICATIONS FOR TYPE-APPROVAL OF A VEHICLE

WITH RESPECT TO ELECTROMAGNETIC COMPATIBILITY

(See 3.1.2)

The following information, if applicable, shall be supplied in triplicate and shall include

a list of contents.

Any drawings shall be supplied in appropriate scale and in sufficient detail on size A 4

or in a folder of A4 format.

Photographs, if any, shall show sufficient detail.

If the systems, components or separate technical units have electronic controls,

information concerning their performance shall be supplied.

GENERAL

1 Make (trade name of manufacturer):

2 Type:

3 Category of vehicle:

4 Name and address of manufacturer:

Name and address of authorized representative, if any:

5 Address (es) of assembly plant(s):

GENERAL CONSTRUCTION CHARACTERISTICS OF THE VEHICLE

6 Photograph(s) and/or drawing(s) of a representative vehicle:

7 Position and arrangement of the engine:

POWER PLANT

8 Manufacturer:

9 Manufacturer's engine code as marked on the engine:

10 Internal combustion engine:

11 Working principle: positive ignition/compression ignition,

four-stroke/two stroke

12 Number and arrangement of cylinders:


44/149

13 FUEL FEED:

14 By fuel injection (compression ignition only): yes/no

15 Electronic control unit:

16 Make(s):

17 Description of the system:

18 By fuel injection (positive ignition only): yes/no

19 Electrical system:

20 Rated voltage: (V, positive/negative ground)

21 Generator:

22 Type:

23 Ignition:

24 Make(s):

25 Type(s):

26 Working principle:

27 LPG fuelling system: yes/no

28 Electronic engine management control unit for LPG fuelling:

29 Make(s):

30 Type(s):

31 CNG fuelling system: yes/no

32 Electronic engine management control unit for CNG fuelling:

33 Make(s):

34 Type(s):

35 Electric motor:

36 Type (winding, excitation):

37 Operating voltage:

Gas fuelled engines (in the case of systems laid-out in a different manner, supply

equivalent information)


45/149

38 Electronic control unit (ECU):

39 Make(s):

40 Type(s):

TRANSMISSION

41 Type (mechanical, hydraulic, electric, etc.):

42 A brief description of the electrical/electronic components (if any):

SUSPENSION


STEERING


BRAKES

45 Anti-lock braking system: yes/no/optional

46 For vehicles with anti-lock systems, description of system operation

(including any electronic parts), electric block diagram, hydraulic or

pneumatic circuit plan:

BODYWORK

47 Type of bodywork:

48 Materials used and methods of construction:

49 Windscreen and other windows:

50 Rear-view mirrors (state for each mirror):

A brief description of the electronic components (if any) of the adjustment

system:

51 Safety belts and/or other restraint systems:


53 Suppression of radio interference:

54 Description and drawings/photographs of the shapes and constituent materials

of the part of the body forming the engine compartment and the part of the

passenger compartment nearest to it:


46/149

55 Drawings or photographs of the position of the metal components housed in

the engine compartment (e.g. heating appliances, spare wheel, air filter,

steering mechanism, etc.):

56 Table and drawing of radio interference control equipment:

57 Particulars of the nominal value of the direct current resistance and, in the case

of resistive ignition cables, of their nominal resistance per meter:

LIGHTING AND LIGHT SIGNALLING DEVICES

58 A brief description of electrical/electronic components other than lamps

(if any):

MISCELLANEOUS

59 Devices to prevent unauthorized use of the vehicle:

60 A brief description of the electrical/electronic components

(if any):

61 Table of installation and use of RF transmitters in the vehicle(s), if applicable

(see paragraph 3.1.8. of this Standard):

frequency bands [Hz] max. output power [W] antenna position at

vehicle,

specific conditions for

installation and/or use

62

Vehicle equipped with 24 GHz short-range radar equipment: yes/no/optional

The application for type approval shall also include, where appropriate:

Appendix 1:

A list with make(s) and type(s) of all electrical and/or electronic components

concerned by this standard (see paragraphs 2.9. and 2.10. of this standard) and

not previously listed.

Appendix 2:

Schematics or drawing of the general arrangement of electrical and/or

electronic components (concerned by this Standard) and the general wiring

harness arrangement.

Appendix 3:

Description of vehicle chosen to represent the type:

Body style:


47/149

Wheelbase:

Appendix 4:

Relevant test report(s) supplied by the manufacturer from a test laboratory

accredited to ISO 17025 and recognized by the Test Agency for the purpose of

drawing up the type approval certificate.

63 Charger: on board/external/without:

64 Charging current: direct current / alternating current (number of

phases/frequency):

65 Maximal nominal current (in each mode if necessary):

66 Nominal charging voltage:

67 Basic vehicle interface functions: ex: L1/L2/L3/N/E/control pilot:

68 Minimum Rsce value (see paragraph 7.3.)

69 Charging cable delivered with the vehicle: yes/no

70 If charging cable delivered with the vehicle:

Length (m).

Cross sectional area (mm²)

71 Portable charger delivered with the vehicle: yes/no

72 Portable Charger Make, Model, Part Number


48/149

ANNEX 1B

TECHNICAL SPECIFICATIONS FOR TYPE-APPROVAL OF AN

ELECTRIC/ELECTRONIC SUB-ASSEMBLY WITH RESPECT TO

ELECTROMAGNETIC COMPATIBILITY

(See 3.1.3)

The following information, if applicable, shall be supplied in triplicate and must include

a list of contents. Any drawings shall be supplied in appropriate scale and in sufficient

detail on size A4 or on a folder of A4 format. Photographs, if any, shall show sufficient

detail.

If the systems, components or separate technical units have electronic controls,

information concerning their performance shall be supplied.

1 Make (trade name of manufacturer):

2 Type:

3 Means of identification of type, if marked on the component/separate

technical unit:

3.1 Location of that marking:

4 Name and address of manufacturer:

Name and address of authorized representative, if any:

5 In the case of components and separate technical units, location and method of

affixing of the approval mark:

6 Address(s) of assembly plant(s):

7 This ESA shall be approved as a component/STU

8 Any restrictions of use and conditions for fitting:

9 Electrical system rated voltage: (V, positive/negative 2/ ground.)

Appendix 1:

Description of the ESA chosen to represent the type (electronic block diagram

and list of main component constituting the ESA (e.g. make and type of

microprocessor, crystal, etc.).

Appendix 2:

Relevant test report(s) supplied by the manufacturer from a test laboratory

accredited to ISO 17025 and recognized by the Test Agency for the purpose of

drawing up the type approval certificate."


49/149

10 Charger: on board/external / portable

11 Charging current: direct current / alternating current (number of phases /

frequency)

12 Maximal nominal current (in each mode if necessary)

13 Nominal charging voltage

14 Basic ESA interface functions: ex. L1 / L2 / L3 / N / PE / control pilot

15 Minimum Rsce value (see paragraph 6.11. of this Standard)


50/149

ANNEX 2

METHOD OF MEASUREMENT OF RADIATED BROADBAND

ELECTROMAGNETIC EMISSIONS FROM VEHICLES

(See 5.2.1 and 6.2)

1.0 GENERAL

1.1 The test method described in this Annex shall only be applied to vehicles.

This method concerns both configurations of the vehicle:

(a) Other than "REESS charging mode coupled to the power grid".

(b) "REESS charging mode coupled to the power grid"

1.2 Test Method

This test is intended to measure the broadband emissions generated by

electrical or electronic systems fitted to the vehicle (e.g. ignition system or

electric motors).

If not otherwise stated in this annex the test shall be performed according to

CISPR 12 (Amendment 1 fifth edition 2005).

2.0 VEHICLE STATE DURING TESTS

2.1 Vehicle in configuration other than "REESS charging mode coupled to the

power grid".

2.1.1 Engine

The engine shall be in operation according to CISPR 12.

2.1.2 Other vehicle systems

All equipment capable of generating broadband emissions which can be

switched on permanently by the driver or passenger should be in operation in

maximum load, e.g. wiper motors or fans. The horn and electric window motors

are excluded because they are not used continuously.

For vehicles equipped with an internal combustion engine, the engine shall be

in operation according to CISPR 12, clause 5.3.2. Typically for single cylinder

engines, the engine speed shall be 2500 + 10% rpm and for multi-cylinder

(>1 cylinder) engines, the engine speed shall be 1500 + 10% rpm.

For vehicles equipped with an electric propulsion motor, the vehicle shall be

driven on a dynamometer without a load, or on non-conductive axle stands,

with a constant speed of 40 km/h, or the maximum speed, if this is less than

40 km/h.


51/149

2.2 Vehicle in configuration "REESS charging mode coupled to the power grid".

The state of charge (SOC) of the traction battery shall be kept between

20 per cent and 80 per cent of the maximum SOC during the whole frequency

range measurement (this may lead to split the measurement into different

sub-bands with the need to discharge the vehicle's traction battery before

starting the next sub-bands). If the current consumption can be adjusted, then

the current shall be set to at least 80 per cent of its nominal value.

The test set-up for the connection of the vehicle in configuration "REESS

charging mode coupled to the power grid" is shown in Figures 3a to 3h

(depending of AC or DC power charging mode, location of charging plug and

charging with or without communication) of Appendix 1 to this annex

2.3 Charging station / Power mains

The charging station may be placed either in the test location or outside the test

location.

Note 1: If the communication between the vehicle and the charging station

could be simulated, the charging station may be replaced by the supply from

power mains.

In both case, duplicated power mains and communication lines socket(s) shall

be placed in the test location with the following conditions:

(a) It shall be placed on the ground plane.

(b) The length of the harness between the power mains/communication lines

socket and the AN(s)/IS(s) shall be kept as short as possible.

(c) The harness between the power mains/communication lines socket and the

AN(s)/IS(s) shall be placed as close as possible to the ground plane.

Note 2: The power mains and communication lines socket(s) should be filtered.

If the charging station is placed inside the test location, then the harness

between charging station and the power mains / communication lines socket

shall be placed with the following conditions:

(a) The harness on charging station side shall hang vertically down to the

ground plane.

(b) The extraneous length shall be placed as close as possible to the ground

plane and "Z-folded" if necessary.

Note 3: The charging station should be placed outside the beam width of the

receiving antenna.

2.4 Artificial networks


52/149

The AN(s) shall be mounted directly on the ground plane. The cases of the

AN(s) shall be bonded to the ground plane.

The measuring port of each AN shall be terminated with a 50-ohm load.

The AN shall be placed as defined in Figures 3a to 3h.

2.5 Impedance stabilization

Communication lines shall be applied to the vehicle through IS(s).

The impedance stabilization (IS) to be connected in the network and

communication cables is defined in CISPR 32, paragraph C.4.1.2.

The IS(s) shall be mounted directly on the ground plane. The case of the IS(s)

shall be bonded to the ground plane.

The measuring port of each IS shall be terminated with a 50 Ω load.

The IS shall be placed as defined in Figures 3e to 3h.

2.6 Power charging / communication cable

The power charging / communication cable shall be placed in a straight line

between the AN(s) / IS(s) and the vehicle charging plug. The projected cable

length shall be 0.8 m (+0.2/-0 m).

If the length of the cable is longer than 1 m, the extraneous length shall be

"Z-folded" in less than 0.5 m width.

The charging / communication cable at vehicle side shall hang vertically at a

distance of 100 mm (+200/-0 mm) from the vehicle body.

The whole cable shall be placed on a non-conductive, low relative permittivity

(dielectric-constant) material (εr ≤ 1.4), at 100 mm (±25 mm) above the ground

plane

3.0 MEASURING LOCATION

3.1 As an alternative to the requirements of CISPR 12 (amendment 1, fifth

edition 2005) for vehicles of category L the test surface may be any location

that fulfils the conditions shown in the figure 1 in the appendix to this annex. In

this case the measuring equipment must lie outside the part shown in the figures

1 and 2 of Appendix 1 to this annex.

53/149

3.2 Enclosed test facilities may be used if correlation can be shown between the results obtained in the enclosed test facility and

those obtained at an outdoor site. Enclosed test facilities do not need to meet the dimensional requirements of the outdoor site

other than the distance from the antenna to the vehicle and the height of the antenna.

AIS

-004 (P

art 3

) (Rev

.1)

4.0 TEST REQUIREMENTS

4.1 The limits apply throughout the frequency range 30 to 1,000 MHz for measurements performed in a semi anechoic chamber or

an outdoor test site.

4.2 Measurements can be performed with either quasi-peak or peak detectors.

The limits given in paragraphs 5.2 and 5.5 of this standard are for quasi-peak detectors. If peak detectors are used a correction

factor of 20 dB as defined in CISPR 12 (amendment 1, fifth edition 2005) shall be applied.

4.3 The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in

Table 1 and Table 2

Table 1

Spectrum analyser parameters

Frequency Range,

MHz

Peak detector Quasi-peak detector Average detector

RBW at -3 dB Scan time RBW at -6 dB Scan time RBW at -3 dB Scan time

30 to 1,000 100/120 kHz 100 ms/MHz 120 kHz 20 s/MHz 100/120 kHz 100 ms/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution

bandwidth (RBW).

54/149

Table 2

Scanning receiver parameters

Frequency Range,

MHz


BW at -6

dB

Step Size (a) Dwell

time

BW at -6

dB

Step size (a) Dwell

time

BW at -6

dB

Step size (a) Dwell

time

30 to 1,000 120 Hz 50 kHz 5 ms 120 kHz 50 kHz 1 s 120 kHz 50 kHz 5 ms

(a) For purely broadband disturbances, the maximum frequency step size may be increased up to a value not greater than the

bandwidth value.

AIS

-004 (P

art 3

) (Rev

.1)


55/149

4.4 Measurements

The Test Agency shall perform the test at the intervals specified in the

CISPR 12 (amendment 1, fifth edition 2005) standard throughout the

frequency range 30 to 1,000 MHz.

Alternatively, if the manufacturer provides measurement data for the whole

frequency band from a test laboratory accredited to the applicable parts of

ISO 17025 and recognized by the Test Agency, the Test Agency may divide

the frequency range in 14 frequency bands 30 – 34, 34 – 45, 45 – 60,

60 – 80, 80 – 100, 100 – 130, 130 – 170, 170 – 225, 225 – 300, 300–400, 400

– 525, 525 – 700, 700 – 850, 850 – 1,000 MHz and perform tests at the 14

frequencies giving the highest emission levels within each band to confirm

that the vehicle meets the requirements of this annex.

In the event that the limit is exceeded during the test, investigations shall be

made to ensure that this is due to the vehicle and not due to background

radiation.

4.5 Readings

The maximum of the readings relative to the limit (horizontal and vertical

polarization and antenna location on the left and right-hand sides of the

vehicle) in each of the 14 frequency bands shall be taken as the characteristic

reading at the frequency at which the measurements were made.


56/149

ANNEX 2 - APPENDIX 1

Figure 1

Clear Horizontal Surface Free of Electromagnetic Reflection

delimitation of the Surface Defined by an Ellipse


57/149

Figure 2

Position of Antenna in Relation to the Vehicle

Figure 2a

Dipole antenna in position to measure the vertical radiation

components

Figure 2b

Dipole antenna in position to measure the horizontal radiation

components


58/149

Figure 3

Vehicle in configuration "REESS charging mode" coupled to the power

grid:

Example of test set-up for vehicle with plug located on vehicle side (AC

powered without communication)

Figure 3a – Front View

Figure 3b – Top View


grid


59/149

Example of test setup for vehicle with plug located front / rear of vehicle

(AC powered without communication)

Figure 3c – Front View


grid

Example of test set-up for vehicle with plug located on vehicle side (AC or

DC powered with communication)

Figure 3d – Top View


60/149

Figure 3e – Front View


grid

Example of test setup for vehicle with plug located front/rear of the vehicle

(AC or DC powered with communication)

Figure 3f – Top View


61/149

Figure 3g – Front View

Figure 3h – Top View


62/149

ANNEX 3

METHOD OF MEASUREMENT OF RADIATED NARROWBAND

ELECTROMAGNETIC EMISSIONS FROM VEHICLES

(See 5.3.1)

1.0 GENERAL

1.1 The test method described in this annex shall only be applied to vehicles.

This method concerns only the configuration of the vehicle other than

"REESS charging mode coupled to the power grid".

1.2 Test Method

This test is intended to measure the narrowband electromagnetic emissions

such as might emanate from microprocessor-based systems or other

narrowband source.


CISPR 12 (amendment 1, fifth edition 2005) or to CISPR 25 (second

edition 2002).

1.3 As an initial step the levels of emissions in the FM frequency band

(76 to 108 MHz) shall be measured at the vehicle broadcast radio antenna

with an average detector. If the level specified in paragraph 5.3.2.4 of this

standard is not exceeded, then the vehicle shall be deemed to comply with

the requirements of this annex in respect of that frequency band and the full

test shall not be carried out.

1.4 As an alternative for vehicles of category L the measurement location can be

chosen according to Annex 2, paragraphs 3.1 and 3.2.


2.1 The ignition switch shall be switched on. The engine shall not be operating.

2.2 The vehicle's electronic systems shall all be in normal operating mode with

the vehicle stationary.

2.3 All equipment which can be switched on permanently by the driver or

passenger with internal oscillators > 9 kHz or repetitive signals should be in

normal operation.


3.1 The limits apply throughout the frequency range 30 to 1,000 MHz for

measurements performed in a semi anechoic chamber or an outdoor test site.


63/149

3.2 Measurements shall be performed with an average detector.

3.3 The measurements shall be performed with a spectrum analyser or a

scanning receiver. The parameters to be used are defined in Table 1 and

Table 2.

Table 1


Frequency

range

MHz

Peak detector Quasi-peak

detector

Average detector

RBW at

-3 dB

Scan

time

RBW

at -6 dB

Scan

time

RBW at

-3 dB

Scan time

30 to 1,000 100/120

kHz

100

ms/MHz

120 kHz 20

s/MHz

100/120

kHz

100 ms/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall

be at least three times the resolution bandwidth (RBW).

Table 2


Frequency

range MHz


BW

at -6

dB

Step

size (a)

Dwe

ll

time

BW

at -6

dB

Step

size (a)

Dwe

ll

time

BW

at -6

dB

Step

size (a)

Dwell time

30 to 1,000 120

kHz

50

kHz

5 ms 120

kHz

50

kHz

1 s 120

kHz

50

kHz

5 ms

(a) For purely broadband disturbances, the maximum frequency step size may be

increased up to a value not greater than the bandwidth value.

3.4 Measurements


CISPR 12 (amendment 1, fifth edition 2005) standard throughout the

frequency range 30 to 1,000 MHz.



ISO 17025 and recognized by the Test Agency, the Test Agency

may divide the frequency range in 14 frequency bands 30 – 34, 34 – 45, 45

– 60, 60 – 80, 80 – 100, 100 – 130, 130 – 170, 170 – 225, 225 – 300,

300– 400, 400 – 525, 525 – 700, 700 – 850, 850 – 1,000 MHz and perform

tests at the 14 frequencies giving the highest emission levels within each

band to confirm that the vehicle meets the requirements of this annex.


64/149


made to ensure that this is due to the vehicle and not due to background

radiation including broadband radiation from any ESA.

3.5 Readings

The maximum of the readings relative to the limit (horizontal and vertical

polarization and antenna location on the left and right-hand sides of the

vehicle) in each of the 14 frequency bands shall be taken as the characteristic



65/149

ANNEX 4

METHOD OF TESTING FOR IMMUNITY OF VEHICLES TO

ELECTROMAGNETIC RADIATION

(See 5.4.1 and 6.7) 1.0 GENERAL

1.1 The test method described in this annex shall only be applied to vehicles.

This method concerns both configurations of vehicle:

(a) Other than "REESS charging mode coupled to the power grid".

(b) "REESS charging mode coupled to the power grid".

1.2 Test Method

This test is intended to demonstrate the immunity of the vehicle electronic

systems. The vehicle shall be subjected to electromagnetic fields as described in

this annex. The vehicle shall be monitored during the tests.


ISO 11451-2, third edition 2005.

1.3 Alternative test methods

The test may be alternatively performed in an outdoor test site for all vehicles. The

test facility shall comply with (national) legal requirements regarding the

emission of electromagnetic fields.

If a vehicle is longer than 12 m and/or wider than 2.60 m and/or higher

than 4.00 m, BCI (bulk current injection) method according to ISO 11451-4

(first edition 1995) can be used in the frequency range 20 to 2,000 MHz with

levels defined in paragraph 5.7.2.1 of this standard.


2.1 Vehicle in configuration other than "REESS charging mode coupled to the power

grid

2.1.1 The vehicle shall be in an unladen condition except for necessary

test equipment.

2.1.1.1 The engine shall normally turn the driving wheels at a steady speed of 50 km/h if

there is no technical reason due to the vehicle to define a

different condition. For vehicles of categories L1, L5 and L7 the steady speed

shall normally be turned at 25 km/h. The vehicle shall be on an appropriately

loaded dynamometer or alternatively supported on insulated axle stands with

minimum ground clearance if no dynamometer is available. Where appropriate,

transmission shafts, belts or chains may be disconnected (e.g. trucks, two- and

three wheel vehicles).


66/149

2.1.1.2 Basic vehicle conditions

The paragraph defines minimum test conditions (as far as applicable) and

failures criteria for vehicle immunity tests. Other vehicle systems, which can

affect immunity related functions must be tested in a way to be agreed between

manufacturer and Test Agency.

"50 km/h cycle" vehicle test

conditions

Failure criteria

Vehicle speed 50 km/h (respectively

25 km/h for L1, L5 and L7 vehicles)

20 per cent (vehicle driving the

rollers). If the vehicle is equipped

with a cruise control system, it shall

be operational.

Speed variation greater than 10 per

cent of the nominal speed. In case of

automatic gearbox: change of gear ratio

inducing a speed variation greater

than 10 per cent of the nominal speed.

Dipped beams ON (manual mode) Lighting OFF

Front wiper ON (manual mode)

maximum speed

Complete stop of front wiper

Direction indicator on driver's side

ON

Frequency change (lower than 0.75 Hz or

greater than 2.25 Hz). Duty cycle change

(lower than 25 per cent or greater

than 75 per cent).

Adjustable suspension in normal

position

Unexpected significant variation

Driver's seat and steering wheel in

medium position

Unexpected variation greater than 10 per

cent of total range

Alarm unset Unexpected activation of alarm

Horn OFF Unexpected activation of horn

Airbag and safety restraint systems

operational with inhibited passenger

airbag if this function exists

Unexpected activation

Automatic doors closed Unexpected opening

Adjustable endurance brake lever in

normal position


"Brake cycle" vehicle test

conditions Failure criteria

To be defined in brake cycle test plan.

This must include operation of the

brake pedal (unless there are technical

reasons not to do so) but not

necessarily an anti-lock brake system

action.

Stop lights inactivated during cycle

Brake warning light ON with loss of

function.



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2.1.1.3. All equipment which can be switched on permanently by the driver or

passenger should be in normal operation.

2.1.1.4. All other systems which affect the driver's control of the vehicle shall be (on)

as in normal operation of the vehicle.

2.1.2 If there are vehicle electrical/electronic systems which form an integral part

of the direct control of the vehicle, which will not operate under the

conditions described in paragraph 2.1., it will be permissible for the

manufacturer to provide a report or additional evidence to the Test Agency

that the vehicle electrical/electronic system meets the requirements of this

standard. Such evidence shall be retained in the type approval

documentation.

2.1.3 Only non-perturbing equipment shall be used while monitoring the vehicle.

The vehicle exterior and the passenger compartment shall be monitored

to determine whether the requirements of this annex are met (e.g. by using

(a) video camera(s), a microphone, etc.).

2.2 Vehicle in configuration "REESS charging mode coupled to the power grid".

2.2.1 The vehicle shall be in an unladen condition except for necessary test

equipment.

2.2.1.1 The vehicle shall be immobilized, engine OFF and in charging mode.

2.2.1.2 Basic vehicle conditions


failures criteria for vehicle immunity tests. Other vehicle systems, which can

affect immunity related functions, shall be tested in a way to be agreed

between manufacturer and Test Agency.

"RESS charging mode" vehicle test

conditions Failure criteria

The RESS shall be in charging mode.

The RESS State of charge (SOC) shall

be kept between 20 percent and 80

percent of the maximum SOC during

the whole frequency range

measurement (this may lead to split

the measurement in different

sub-bands with the need to discharge

the vehicle’s traction battery before

starting the next sub-bands). If the

current consumption can be adjusted,

then the current shall be set to at least

20 percent of its nominal value.

Vehicle sets in motion.


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2.2.1.3 All other equipment which can be switched on permanently by the driver or

passenger should be OFF.

2.2.2 Only non-perturbing equipment shall be used while monitoring the vehicle.

The vehicle exterior and the passenger compartment shall be monitored to

determine whether the requirements of this annex are met (e.g. by using

(a) video camera(s), a microphone, etc.).

2.2.3 The test set-up for the connection of the vehicle in configuration "REESS

charging mode coupled to the power grid" is shown in Figures 4a to 4h

(depending of AC or DC power charging mode, location of charging plug

and charging with or without communication) of Appendix 1 to this annex.

2.3 Charging station / Power mains

The charging station may be placed either in the test location or outside the

test location.

Note 1: If the communication between the vehicle and the charging station

could be simulated, the charging station may be replaced by the supply from

power mains.

In both case duplicated power mains and communication lines socket(s)

shall be placed in the test location with the following conditions:

(a) It shall be placed on the ground plane;

(b) The length of the harness between the power mains / communication

lines socket and the AN(s) / IS(s) shall be kept as short as possible;

(c) The harness between the power mains / communication lines socket and

the AN(s) / IS(s) shall be placed as close as possible of the ground plane.

Note 2: The power mains and communication lines socket(s) should be

filtered. If the charging station is placed inside the test location, then

harness between charging station and the

power mains / communication lines socket shall be placed with the

following conditions:

(a) The harness at charging station side shall hang vertically down to the

ground plane;

(b) The extraneous length shall be placed as close as possible of the ground

plane and "Z-folded" if necessary.

Note 3: The charging station should be placed outside the beam width of the

emitting antenna.


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2.4 Artificial networks



The measuring port of each AN shall be terminated with a 50 Ω load.

The AN shall be placed as defined in Figures 4a to 4h.



The impedance stabilization (IS) to be connected in the network and

communication cables is defined in CISPR 32 paragraph C.4.1.2.

The IS(s) shall be mounted directly on the ground plane. The case of the

IS(s) shall be bonded to the ground plane.

The measuring port of each IS shall be terminated with a 50 Ω load.

The IS shall be placed as defined in Figures 4e to 4h.

2.6 Power charging / Communication cable

The power charging / communication cable shall be placed in a straight line

between the AN(s) / IS(s) and the vehicle charging plug. The projected cable

length shall be 0.8 m (+0.2/-0 m).

If the length of the cable is longer than 1 m, the extraneous length shall be

"Z-folded" in less than 0.5 m width.

The charging / communication cable at vehicle side shall hang vertically at a

distance of 100 mm (+200/-0 mm) from the vehicle body.

The whole cable shall be placed on a non-conductive, low relative

permittivity (dielectric-constant) material (εr ≤ 1.4), at 100 mm (±25 mm)

above the ground plane.

3.0 REFERENCE POINT

3.1 For the purposes of this annex, the reference point is the point at which the

field strength shall be established and shall be defined as follows:

3.2 For category L7, M, N, T vehicles according to ISO 11451-2, third

edition 2005.

3.3 For category L vehicles (except L7):

3.3.1 At least 2 m horizontally from the antenna phase centre or at least 1 m

vertically from the radiating elements of a transmission-line-system (TLS);


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3.3.2 On the vehicle's centre line (plane of longitudinal symmetry);

3.3.3 At a height of 1.0 ± 0.05 m above the plane on which the vehicle rests

or 2.0 ± 0.05 m if the minimum height of the roof of any vehicle in the model

range exceeds 3.0m,

3.3.4 Either at 1.0 ± 0.2 m behind the vertical centerline of the vehicle's front

wheel (point C in figure 1 of Appendix 1 to this annex) in the case of

three-wheeled vehicles, or at 0.2 ± 0.2 m behind the vertical centerline of the

vehicle's front wheel (point D in figure 2 of Appendix 1 to this annex) in the

case of two-wheeled vehicles.

3.3.5 If it is decided to radiate the rear of the vehicle, the reference point shall be

established as in paragraphs 3.3.1. to 3.3.4. The vehicle shall then be

installed facing away from the antenna and positioned as if it had been

horizontally rotated 180 around its centre point, i.e. such that the distance

from the antenna to the nearest part of the outer body of the vehicle remains

the same. This is illustrated in figure 3 of Appendix 1 to this annex.


4.1 Frequency range, dwell times, polarization

The vehicle shall be exposed to electromagnetic radiation in the 20 to 2,000

MHz frequency ranges in vertical polarization.

The test signal modulation shall be:

(a) AM (amplitude modulation), with 1 kHz modulation and 80 percent

modulation depth in the 20 to 800 MHz frequency range, and

(b) PM (pulse modulation), t on 577 µs, period 4,600 µs in the 800 to 2,000

MHz frequency range,

if not otherwise agreed between Test Agency and vehicle manufacturer.

Frequency step size and dwell time shall be chosen according to


4.1.1 The Test Agency shall perform the test at the intervals specified in

ISO 11451-1, third edition 2005 throughout the frequency

range 20 to 2,000 MHz.

Alternatively, if the manufacturer provides measurement to data for the

whole frequency band from a test laboratory accredited to the applicable

parts of ISO 17025 and recognized by the Test Agency, the Test Agency

may choose a reduced number of spot frequencies in the range, e.g. 27, 45,

65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750, 900, 1,300,

and 1,800 MHz to confirm that the vehicle meets the requirements of this

annex.


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If a vehicle fails the test defined in this annex, it must be verified as having

failed under the relevant test conditions and not as a result of the generation

of uncontrolled fields.

5.0 GENERATION OF REQUIRED FIELD STRENGTH

5.1 Test methodology

5.1.1 The substitution method according to ISO 11451-1, third edition 2005 shall

be used to establish the test field conditions.

5.1.2 Calibration

For TLS one field probe at the facility reference point shall be used.

For antennas four field probes at the facility reference line shall be used.

5.1.3 Test phase

The vehicle shall be positioned with the centre line of the vehicle on the

facility reference point or line. The vehicle shall normally face a fixed

antenna. However, where the electronic control units and the associated

wiring harness are predominantly in the rear of the vehicle, the test should

normally be carried out with the vehicle facing away from the antenna.

In the case of long vehicles (i.e. excluding vehicles of categories L, M1 and

N1), which have electronic control units and associated wiring harness

predominantly towards the middle of the vehicle, a reference point may be

established based on either the right side surface or the left side surface of the

vehicle. This reference point shall be at the midpoint of the vehicle's length

or at one point along the side of the vehicle chosen by the manufacturer in

conjunction with the Test Agency after considering the distribution of

electronic systems and the layout of any wiring harness.

Such testing may only take place if the physical construction of the chamber

permits. The antenna location must be noted in the test report.


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ANNEX 4 – APPENDIX 1

Figure 1

Figure 2


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Figure 3


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Figure 4

Vehicle in configuration "REESS charging mode coupled to the power grid"

Example of test set-up for vehicle with plug located on the vehicle side (AC power

charging without communication)




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Example of test set-up for vehicle with plug located front / rear of vehicle (AC power

charging without communication)




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Example of test set-up for vehicle with plug located on vehicle side (AC or DC power

charging with communication)

Figure 4e – Front View

Figure 4f – Top View


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Example of test set-up for vehicle with plug located front / rear of the vehicle (AC or DC

power charging with communication)

Figure 4g – Front View

Figure 4h – Top View


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ANNEX 5

(See 5.5.1 and 6.10)

METHOD OF MEASUREMENT OF

RADIATED BROADBAND ELECTROMAGNETIC EMISSIONS FROM

ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES

1.0 GENERAL

1.1 The test method described in this annex may be applied to ESAs which may be

subsequently fitted to vehicles, which comply with Annex 2.

1.2 This method concerns both kinds of ESA:

(a) Other ESAs than involved in "REESS charging mode coupled to the power

grid".

(b) ESAs involved in "REESS charging mode coupled to the power grid".

Test method

This test is intended to measure broadband electromagnetic emissions from

ESAs (e.g. ignition systems, electric motor, etc.).


CISPR 25 (second edition 2002).

2.0 ESA STATE DURING TESTS

2.1 The ESA under test shall be in normal operation mode, preferably in maximum

load.

ESAs involved in "REESS charging mode coupled to the power grid" shall be in

charging mode.



range measurement (this may lead to split the measurement in different

sub-bands with the need to discharge the vehicle's traction battery before starting

the next sub-bands)

If the test is not performed with a REESS the ESA should be tested at rated

current. If the current consumption can be adjusted, then the current shall be set

to at least 80 per cent of its nominal value.

3.0 TEST ARRANGEMENTS

3.1 For ESA other than involved in "REESS charging mode coupled to the power

grid" the test shall be performed according to CISPR 25 (second edition 2002)

clause 6.4. - ALSE method.


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3.2 For ESAs in configuration "REESS charging mode coupled to the power grid"

the test arrangement shall be according to Figure 2 of the appendix to this annex.

3.2.1 The shielding configuration shall be according to the vehicle series

configuration. Generally, all shielded High Voltage (HV) parts shall be properly

connected with low impedance to ground (e. g. AN, cables, connectors etc.).

ESAs and loads shall be connected to ground. The external HV power supply

shall be connected via feed-through-filtering.

3.2.2 Unless otherwise specified the length of the Low Voltage (LV) harness and the

HV harness parallel to the front edge of the ground plane shall be

1,500 mm (±75 mm). The total length of the test harness including the connector

shall be 1,700 mm (+300/-0 mm). The distance between the LV harness and the

HV harness shall be 100 mm (+100/-0 mm).

3.2.3 All of the harnesses shall be placed on a non-conductive, low relative

permittivity material (εr ≤ 1.4), at 50 mm (±5 mm) above the ground plane.

3.2.4 Shielded supply lines for HV+ and HV- line and three phase lines may be

coaxial cables or in a common shield depending on the used plug system.

The original HV-harness from the vehicle may be used optionally.

3.2.5 Unless otherwise specified, the ESA case shall be connected to the ground plane

either directly or via defined impedance.

3.2.6 For onboard chargers, the AC/DC power lines shall be placed the furthest from

the antenna (behind LV and HV harness). The distance between the

AC/DC power lines and the closest harness (LV or HV) shall be 100 mm

(+100/-0 mm).

3.3 Alternative measuring location

As an alternative to an absorber lined shielded enclosure (ALSE) an open area

test site (OATS), which complies with the requirements of CISPR 16-1-4 may

be used (see appendix to this annex).

3.4 Ambient

To ensure that there is no extraneous noise or signal of a magnitude sufficient to

affect materially the measurement, measurements shall be taken before or after

the main test. In this measurement, the extraneous noise or signal shall be at

least 6 dB below the limits of interference given in paragraph 5.5.2.1 of this

standard, except for intentional narrowband ambient transmissions.




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4.2 Measurements can be performed with either quasi-peak or peak detectors.

AIS

-004 (P

art 3

) (Rev

.1)

The limits given in paragraphs 5.2 and 5.5 of this standard are for quasi-peak detectors.

If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 (fifth edition 2001) shall be applied.


Table 1 and Table 2.

Table 1


Frequency

range

MHz


RBW at -3 dB Scan time RBW at -6 dB Scan tiem RBW at -3 dB Scan time


Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth

(RBW).

Table 2


Frequency

range

MHz


BW at

-6 dB

Step

size

Dwell time BW at

-6 dB

Step size (a) Dwell

time

BW at -6 dB Step size (a) Dwell time

30 to 1,000 120

kHz

50 kHz 5 ms 120

kHz

50 kHz 1 s 120 kHz 50 kHz 5 ms

(a) For purely broadband disturbances, the maximum frequency step size may be increased up to a value not greater than the bandwidth value.

Note: For emissions generated by brush commutator motors without an electronic control unit, the maximum step size may be increased up to five

times the bandwidth.


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4.4 Measurements


CISPR 25 (second edition 2002) standard throughout the frequency




ISO 17025 and recognized by the Test Agency, the Test Agency may

divide the frequency range in 13 frequency bands 30–50, 50-75, 75-100,

100-130, 130-165, 165-200, 200-250, 250-320, 320-400, 400-520, 520-660,

660-820, 820-1,000 MHz and perform tests at

the 13 frequencies giving the highest emission levels within each band to

confirm that the ESA meets the requirements of this annex.


made to ensure that this is due to the ESA and not to background radiation.

4.5 Readings

The maximum of the readings relative to the limit (horizontal / vertical

polarization) in each of the 13 frequency bands shall be taken as the

characteristic reading at the frequency at which the measurements were made.


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15 m minimum radius

Test sample on

ground plane

Antenna

1 m

Figure 1

Open Area Test Site: Electrical/electronic Sub-Assembly test area boundary

level clear area free from electromagnetic reflecting surfaces


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Figure 2

Test configuration for ESAs involved in "REESS charging mode coupled to the

power grid" (example for Bi-conical antenna)

Legend:

1 ESA (grounded locally if required in test

plan)

14 Stimulation and monitoring system

2 LV Test harness 15 HV harness

3 LV Load simulator (placement and ground

connection according to CISPR 25

paragraph 6.4.2.5)

16 HV load simulator

4 Power supply (location optional) 17 HV AN

5 LV Artificial network (AN) 18 HV power supply

6 Ground plane (bonded to shielded enclosure) 19 HV feed-through

7 Low relative permittivity support (εr ≤ 1.4) 25 AC/DC charger harness

8 Biconical antenna 26 AC/DC load simulator (e.g. Programmable Logic

Controller (PLC))

10 High-quality coaxial cable e.g.

double-shielded (50 Ω)

27 50μH Line Impedance Stabilization Network

(LISN) (AC) or HVAN (DC)

11 Bulkhead connector 28 AC/DC power supply

12 Measuring instrument 29 AC/DC feed-through

13 RF absorber material


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ANNEX 6

METHOD OF MEASUREMENT OF

RADIATED NARROWBAND ELECTROMAGNETIC EMISSIONS FROM

ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES

(See 5.6.1)

1.0 GENERAL

1.1 The test method described in this annex shall apply to ESAs, which may be

subsequently fitted to vehicles, which comply, with Annex 3.

This method concerns only ESA other than those involved in "REESS

charging mode coupled to the power grid".

1.2 Test Method

This test is intended to measure the narrowband electromagnetic emissions

such as might emanate from a microprocessor-based system.


CISPR 25 (second edition 2002).


The ESA under test shall be in normal operation mode.


3.1 The test shall be performed according to CISPR 25 (second edition 2002)

clause 6.4. - ALSE method.

3.2 Alternative measuring location

As an alternative to an absorber lined shielded enclosure (ALSE) an open area

test site (OATS) which complies with the requirements of

CISPR 16-1 ( second edition 2002) may be used (see Appendix 1 to

Annex 5).

3.3 Ambient

To ensure that there is no extraneous noise or signal of a magnitude sufficient

to affect materially the measurement, measurements shall be taken before or

after the main test. In this measurement, the extraneous noise or signal shall

be at least 6 dB below the limits of interference given in paragraph 5.6.2.1 of

this standard, except for intentional narrowband ambient transmissions.



measurements performed in semi anechoic chambers or outdoor test sites.

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4.2 Measurements shall be performed with an average detector.

AIS

-004 (P

art 3

) (Rev

.1)

4.3 The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined

in Table 1 and Table 2.

Table 1


Frequency

range

MHz




Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution

bandwidth (RBW).

Table 2


Frequenc

y range

MHz


BW at -6 dB Step size (a) Dwell

time


time


time

30 to

1,000

120 kHz 50 kHz 5 ms 120 kHz 50 kHz 1 s 120 kHz 50 kHz 5 ms


Note: For emissions generated by brush commutator motors without an electronic control unit, the maximum step size may be increased up to

five times the band width.


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4.4 Measurements

The Test Agency shall perform the test at the intervals specified in the CISPR 25

(second edition 2002) standard throughout the frequency




ISO 17025 and recognized by the Test Agency, the Test Agency may

divide the frequency range in 13 frequency bands 30–50, 50-75, 75-100,

100-130, 130-165, 165-200, 200-250, 250-320, 320-400, 400-520, 520-660,

660-820, 820-1,000 MHz and perform tests at the 13 frequencies giving the

highest emission levels within each band to confirm that the ESA meets the

requirements of this annex. In the event that the limit is exceeded during the test,

investigations shall be made to ensure that this is due to the ESA and not due to

background radiation including broadband radiation from the ESA.

4.5 Readings

The maximum of the readings relative to the limit (horizontal/vertical

polarization) in each of the 13 frequency bands shall be taken as the characteristic



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ANNEX 7

(See 5.7.1 and 6.18)

METHOD(S) OF TESTING FOR IMMUNITY OF

ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES TO ELECTROMAGNETIC

RADIATION

1.0 GENERAL

1.1 The test methods described in this annex shall be applied to ESAs.

1.2 Test Methods

This method concerns both kinds of ESA:

(a) Other ESAs than involved in "REESS charging mode coupled to the

power grid";

(b) ESAs involved in "REESS charging mode coupled to the power grid".

1.2.1 ESAs may comply with the requirements of any combination of the

following test methods at the manufacturer's discretion provided that this

results in the full frequency range specified in paragraph 3.1. of this annex

being covered:

(a) Absorber chamber test according to ISO 11452-2, second edition 2004;

(b) TEM cell testing according to ISO 11452-3, third edition 2001;

(c) Bulk current injection testing according to ISO 11452-4,

third edition 2005;

(d) Stripline testing according to ISO 11452-5, second edition 2002;

(e) 800 mm stripline according to paragraph 5 of this annex.

ESAs in configuration "REESS charging mode coupled to the power grid"

shall comply with the requirements of the combination of the Absorber

chamber test according to ISO 11452-2 and Bulk current injection testing

according to ISO 11452-4 at the manufacturer's discretion provided that

these results in the full frequency range specified in paragraph 3.1. of this

annex being covered

(Frequency range and general test conditions shall be based on

ISO 11452-1, third edition 2005).

2.0 STATE OF ESA DURING TESTS

2.1 The test conditions shall be according to ISO 11452-1, third edition 2005.


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2.2 The ESA under test shall be switched on and must be stimulated to be in

normal operation condition. It shall be arranged as defined in this annex

unless individual test methods dictate otherwise.

ESAs involved in "REESS charging mode coupled to the power grid" shall

be in charging mode.

The state of charge (SOC) of the traction battery shall be kept between 20

per cent and 80 per cent of the maximum SOC during the whole frequency



starting the next sub-bands).


current. If the current consumption can be adjusted, then the current shall be

set to at least 20 per cent of its nominal value.

2.3 Any extraneous equipment required to operate the ESA under test shall not

be in place during the calibration phase. No extraneous equipment shall be

closer than 1 m from the reference point during calibration.

2.4 To ensure reproducible measurement results are obtained when tests and

measurements are repeated, the test signal generating equipment and its

layout shall be to the same specification as that used during each appropriate

calibration phase.

2.5 If the ESA under test consists of more than one unit, the interconnecting

cables should ideally be the wiring harnesses as intended for use in the

vehicle. If these are not available, the length between the electronic control

unit and the AN shall be as defined in the standard. All cables in the wiring

harness should be terminated as realistically as possible and preferably with

real loads and actuators.

3.0 GENERAL TEST REQUIREMENTS

3.1 Frequency range, dwell times

Measurements shall be made in the 20 to 2,000 MHz frequency range with

frequency steps according to ISO 11452-1, third edition 2005.

The test signal modulation shall be:

(a) AM (amplitude modulation), with 1 kHz modulation and 80 per cent

modulation depth in the 20 - 800 MHz frequency range;

(b) PM (pulse modulation), t on 577 µs, period 4,600 µs in the 800-2,000 MHz

frequency range,

if not otherwise agreed between Test Agency and ESA manufacturer.

Frequency step size and dwell time shall be chosen according to



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3.2 The Test Agency shall perform the test at the intervals specified in ISO 11452-1

third edition 2005 throughout the frequency range 20 to 2,000 MHz.

Alternatively, if the manufacturer provides measurement to data for the

whole frequency band from a test laboratory accredited to the applicable

parts of ISO 17025 and recognized by the Test Agency, the Test Agency

may choose a reduced number of spot frequencies in the range, e.g. 27, 45,

65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750, 900, 1,300, and

1,800 MHz to confirm that the ESA meets the requirements of this annex.

3.3 If an ESA fails the tests defined in this annex, it must be verified as having

failed under the relevant test conditions and not as a result of the generation

of uncontrolled fields.

4.0 SPECIFIC TEST REQUIREMENTS

4.1 Absorber chamber test

4.1.1 Test method

This test method allows the testing of vehicle electrical/electronic systems

by exposing an ESA to electromagnetic radiation generated by an antenna.

4.1.2 Test methodology

The "substitution method" shall be used to establish the test field conditions

according to ISO 11452-2, second edition 2004.

The test shall be performed with vertical polarization

4.1.2.1 For ESAs in configuration "REESS charging mode coupled to the power

grid" the test arrangement shall be according to Appendix 3 to this annex.

4.1.2.1.1 The shielding configuration shall be according to the vehicle series

configuration. Generally, all shielded HV parts shall be properly connected

with low impedance to ground (e. g. AN, cables, connectors etc.). ESAs and

loads shall be connected to ground. The external HV power supply shall be

connected via feed-through-filtering.

4.1.2.1.2 Unless otherwise specified the length of the LV harness and the HV harness

parallel to the front edge of the ground plane shall be 1,500 mm (±75 mm).

The total length of the test harness including the connector shall be

1,700 mm (+300/-0 mm). The distance between the LV harness and the

HV harness shall be 100 mm (+100/-0 mm).

4.1.2.1.3 All of the harnesses shall be placed on a non-conductive, low relative

permittivity material (εr ≤ 1,4), at 50 mm (±5 mm) above the ground plane.

4.1.2.1.4 Shielded supply lines for HV+ and HV- line and three phase lines may be



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4.1.2.1.5 Unless otherwise specified, the ESA case shall be connected to the ground

plane either directly or via defined impedance.

4.1.2.1.6 For onboard chargers, the AC/DC power lines shall be placed the furthest

from the antenna (behind LV and HV harness). The distance between the

AC/DC power lines and the closest harness (LV or HV) shall be

100 mm (+100/-0 mm).

4.1.2.1.7 Unless otherwise specified, the configuration with the LV harness closer to

the antenna shall be tested.

4.2 TEM cell testing (see Appendix 2 to this annex)

4.2.1 Test method

The TEM (transverse electromagnetic mode) cell generates homogeneous

fields between the internal conductor (septum) and housing (ground plane).


The test shall be performed according to ISO 11452-3, third edition 2001.

Depending on the ESA to be tested the Test Agency shall choose the method

of maximum field coupling to the ESA or to the wiring harness inside the

TEM-cell.

4.3 Bulk current injection testing

4.3.1 Test method

This is a method of carrying out immunity tests by inducing currents

directly into a wiring harness using a current injection probe.


The test shall be performed according to ISO 11452-4, third edition 2005 on

a test bench. As an alternative the ESA may be tested while installed in the

vehicle according to ISO 11451-4 (first edition 1995) with the following

characteristics:

(a) The injection probe shall be positioned in 150 mm distance to the

ESA to be tested;

(b) The reference method shall be used to calculate injected currents from

forward power;

(c) The frequency range of the method is limited by the injection probe

specification.

4.3.2.1. For ESAs in configuration "REESS charging mode coupled to the power


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grid", the test arrangement shall be according to Appendix 4 to this annex.

4.3.2.1.1 The shielding configuration shall be according to the vehicle series

configuration. Generally, all shielded HV parts shall be properly connected

with low impedance to ground (e. g. AN, cables, connectors, etc.). ESAs and

loads shall be connected to ground. The external HV power supply shall be

connected via feed-through-filtering.

4.3.2.1.2. Unless otherwise specified the length of the LV harness and the HV harness

shall be 1,700 mm (+300/-0 mm). The distance between the LV harness and

the HV harness shall be 100 mm (+100/-0 mm).

4.3.2.1.3. All of the harnesses shall be placed on a non-conductive, low relative

permittivity material (εr≤1.4), at (50 ± 5) mm above the ground plane.

4.3.2.1.4. Shielded supply lines for HV+ and HV- line and three phase lines may be



4.3.2.1.5. Unless otherwise specified, the ESA case shall be connected to the ground

plane either directly or via defined impedance.

4.3.2.1.6. Unless otherwise specified the test shall be performed with the injection

probe placed around each of the following harnesses:

(a) Low voltage harness;

(b) High voltage harness;

(c) AC power lines if applicable;

(d) DC power lines if applicable

4.4 Stripline testing

4.4.1 Test method

This test method consists of subjecting the wiring harness connecting the

components in an ESA to specified field strengths.


The test shall be performed according to ISO 11452-5, second

edition 2002.

4.5 800 mm Stripline testing

4.5.1 Test method


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The Stripline consists of two parallel metallic plates separated by 800 mm.

Equipment under test is positioned centrally between the plates and subjected

to an electromagnetic field (see Appendix 1 to this annex).

This method can test complete electronic systems including sensors and

actuators as well as the controller and wiring loom. It is suitable for apparatus

whose largest dimension is less than one third of the plate separation.


4.5.2.1. Positioning of Stripline

The stripline shall be housed in a screened room (to prevent external emissions)

and positioned 2 m away from walls and any metallic enclosure to prevent

electromagnetic reflections. RF absorber material may be used to damp these

reflections. The stripline shall be placed on non-conducting supports at

least 0.4 m above the floor.

4.5.2.2. Calibration of the Stripline

A field-measuring probe shall be positioned within the central one-third of the

longitudinal, vertical and transverse dimensions of the space between the

parallel plates with the system under test absent.

The associated measuring equipment shall be sited outside the screen room. At

each desired test frequency, a level of power shall be fed into the stripline to

produce the required field strength at the antenna. This level of forward power,

or another parameter directly related to the forward power required to define

the field, shall be used for type approval tests unless changes occur in the

facilities or equipment, which necessitate this procedure being repeated.

4.5.2.3. Installation of the ESA under test

The main control unit shall be positioned within the central one third of the

longitudinal, vertical and transverse dimensions of the space between the

parallel plates. It shall be supported on a stand made from non-conducting

material.

4.5.2.4. Main wiring loom and sensor/actuator cables

The main wiring loom and any sensor/actuator cables shall rise vertically from

the control unit to the top ground plate (this helps to maximize coupling with

the electromagnetic field). Then they shall follow the underside of the plate to

one of its free edges where they shall loop over and follow the top of the ground

plate as far as the connections to the stripline feed. The cables shall then be

routed to the associated equipment, which shall be sited in an area outside the

influence of the electromagnetic field, e.g.: on the floor of the screened

room 1 m longitudinally away from the stripline.


93/149


Figure 1

800 mm Stripline Testing

N Type

connector monitor

Details of stripline feed

Brass bracket

Brass bracket

Brass bracket

Brass bracket

N Type

connector

feed

1 = Ground plate

2 = Main loom and sensor/actuator cables

3 = Wooden frame

4 = Driven plate

5 = Insulator

6 = Test object


94/149

Figure 2

800 mm Stripline Dimensions

Earth

Allowed working region

Side view

Allowed working region

Plan view

All Dimensions in mm

Insulating support


95/149


TYPICAL TEM CELL DIMENSIONS

The following table shows the dimensions for constructing a cell with specified upper

frequency limits:

Upper

frequency

(MHz)

Cell form

factor

W : b

Cell form

factor

L/W

Plate

separation

b (cm)

Septum

S (cm)

200 1.69

0.66

56

70

200 1.00 1 60

50


96/149


ABSORBER CHAMBER TEST

Test configuration for ESA's involved in "REESS charging mode coupled to the power

grid". The test shall be performed according to ISO 11452-2.

Legend:

1 ESA (grounded locally if required in test plan) 14 Stimulation and monitoring system

2 LV Test harness 15 HV harness

3 LV Load simulator (placement and ground

connection according to CISPR 25 paragraph

6.4.2.5)

16 HV load simulator

4 Power supply (location optional) 17 HV AN

5 LV Artificial network (AN) 18 HV power supply

6 Ground plane (bonded to shielded enclosure) 19 HV feed-through

7 Low relative permittivity support (εr ≤ 1.4) 25 AC/DC charger harness

8 Biconical antenna 26 AC/DC load simulator (e.g. Programmable Logic

Controller (PLC))

10 High-quality coaxial cable e.g. double-shielded

(50 Ω)

27 50μH Line Impedance Stabilization Network

(LISN) (AC) or HVAN (DC)

11 Bulkhead connector 28 AC/DC power supply

12 Measuring instrument 29 AC/DC feed-through

13 RF absorber material


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BCI TEST

Test configuration for ESAs involved in "REESS charging mode coupled to the power

grid". The test shall be performed according to ISO 11452-4.

Legend:

1 ESA (grounded locally if required in

test plan)

11 HV DC harness

2 LV Test harness 12 HV AN

3 LV supply 13 HV DC load

4 LV LISN 14 HV DC feed-through

5 LV load simulator 15 HV DC load simulator

6 Stimulation and monitoring system 16 HV AC/DC charger harness

7 Low relative permittivity support 17 50 μH LISN (AC) or HV AN (DC)

8 Ground plane 18 HV AC/DC power supply

9 Injection probe 19 HV AC/DC feed-through

10 10 RF signal amplifier and generator 20 2HV AC/DC load simulator (e.g. PLC)


98/149

ANNEX 8

METHOD(S) OF TESTING FOR IMMUNITY TO AND EMISSION OF

TRANSIENTS OF ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES

(See 5.8.1 and 6.19)

1.0 GENERAL

This test method shall ensure the immunity of ESAs to conducted transients

on the vehicle power supply and limit conducted transients from ESAs to the

vehicle power supply.

2.0 IMMUNITY AGAINST DISTURBANCES CONDUCTED ALONG

SUPPLY LINES

Apply the test pulses 1, 2a, 2b, 3a 3b and 4 according to the International

Standard ISO 7637-2: 2004 to the supply lines as well as to other connections

of ESAs which may be operationally connected to supply lines.

3.0 EMISSION OF CONDUCTED DISTURBANCES ALONG SUPPLY

LINES

Measurement according to the International Standard ISO 7637-2: 2004 on

supply lines as well as to other connections of ESAs which may be

operationally connected to supply lines.


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ANNEX 9

METHOD(S) OF TESTING FOR EMISSION OF HARMONICS GENERATED

ON AC POWER LINES FROM VEHICLE

(See 6.3)

1.0 GENERAL

1.1 The test method described in this annex shall be applied to vehicles in

configuration "REESS charging mode coupled to the power grid"

1.2 Test method

This test is intended to measure the level of harmonics generated by vehicle in

configuration "REESS charging mode coupled to the power grid" through its

AC power lines in order to ensure it is compatible with residential, commercial

and light industrial environments.

If not otherwise stated in this annex the test shall be performed according to:

(a) IEC 61000-3-2 for input current in charging mode ≤ 16 A per phase for

class A equipment;

(b) IEC 61000-3-12 for input current in charging mode > 16 A and ≤ 75 A per

phase.


2.1 The vehicle shall be in configuration "REESS charging mode coupled to the

power grid".


20 per cent and 80 per cent of the maximum SOC during the whole time

duration of the measurement (this may lead to the measurement being split into

different time slots with the need to discharge the vehicle’s traction battery

before starting the next time slot). If the current consumption can be adjusted,

then the current shall be set to at least 80 per cent of its nominal value.

The vehicle shall be immobilized, engine OFF.

And all other equipment which can be switched on permanently by the driver

or passenger should be OFF.


3.1 The observation time to be used for the measurements shall be as for

quasi-stationary equipment as defined in IEC 61000-3-2, Table 4.

3.2 The test set-up for single phase vehicle in configuration "REESS charging

mode coupled to the power grid" is shown in Figure 1 of Appendix 1 to this

annex.


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3.3 The test set-up for three-phase vehicle in configuration "REESS charging mode

coupled to the power grid" is shown in Figure 2 of Appendix 1 to this annex.


4.1 The measurements of even and odd current harmonics shall be performed up to

the 40th harmonic.

4.2 The limits for single phase or three-phase "REESS charging mode coupled to

the power grid" with input current ≤ 16 A per phase are given in Table 3 of

paragraph 6.3.2.1. of this Standard.

4.3 The limits for single phase "REESS charging mode coupled to the power grid"

with input current > 16 A and ≤ 75 A per phase are given in Table 4 of


4.4 The limits for three-phase "REESS charging mode coupled to the power grid"

with input current > 16 A and ≤ 75 A per phase are given in Table 5 of


4.5 For three-phase "REESS charging mode coupled to the power grid" with input

current > 16 A and ≤ 75 A per phase, when at least one of the three conditions

a), b) or c) described in paragraph 5.2. of IEC 61000-3-12 is fulfilled, then the

limits given in Table 6 of paragraph 6.3.2.2. of this Standard can be applied.


101/149

Annex 9 – Appendix 1

Figure 1

Vehicle in configuration "REESS charging mode coupled to the power

grid" – Single phase charger test set-up

Figure 2


grid" – Three-phase charger test set-up


102/149

ANNEX 10

METHOD(S) OF TESTING FOR EMISSION OF VOLTAGE CHANGES,

VOLTAGE FLUCTUATIONS AND FLICKER ON AC POWER LINES FROM

VEHICLE

(See 6.4)

1.0 GENERAL


configuration "REESS charging mode coupled to the power grid"

1.2 Test method

This test is intended to measure the level of voltage changes, voltage

fluctuations and flicker generated by vehicle in configuration "REESS charging

mode coupled to the power grid" through its AC power lines in order to ensure it

is compatible with residential, commercial and light industrial environments.


(a) IEC 61000-3-3 for rated current in "REESS charging mode" ≤ 16 A per

phase and not subjected to conditional connection;

(b) IEC 61000-3-11 for rated current in "REESS charging mode" > 16 A and

≤ 75 A per phase and subjected to conditional connection.



power grid".


20 per cent and 80 per cent of the maximum SOC during the whole time

duration of the measurement (this may lead to the measurement being split into

different time slots with the need to discharge the vehicle’s traction battery

before starting the next time slot). If the current consumption can be adjusted,



And all other equipment which can be switched on permanently by the driver or



3.1 The tests for vehicle in configuration "REESS charging mode coupled to the

power grid" with rated current ≤ 16 A per phase and not subjected to conditional

connection shall be performed according to paragraph 4. of IEC 61000-3-3.


103/149

3.2 The tests for vehicle in configuration "REESS charging mode coupled to the

power grid" with rated current > 16 A and ≤ 75 A per phase and subjected to

conditional connection shall be performed according to paragraph 6. of

IEC 61000-3-11.

3.3 The test set-up for vehicle in configuration "REESS charging mode coupled to

the power grid" is shown in Figures 1a and 1b of Appendix 1 to this annex.


4.1 The parameters to be determined in the time-domain are "short duration flicker

value", "long duration flicker value" and "voltage relative variation".

4.2 The limits for vehicle in configuration "REESS charging mode coupled to the

power grid" with input current ≤ 16 A per phase and not subjected to conditional

connection are given in paragraph 6.4.2.1. of this Standard.

4.3 The limits for vehicle in configuration "REESS charging mode coupled to the

power grid" with input current > 16 A and ≤ 75 A per phase and subjected to

conditional connection are given in paragraph 6.4.2.2. of this Standard.


104/149


Figure 1a


grid" – Single phase test set-up

Figure 1b


grid" – Three phase test set-up


105/149

ANNEX 11

METHOD(S) OF TESTING FOR EMISSION OF RADIO FREQUENCY

CONDUCTED DISTURBANCES ON AC OR DC POWER LINES FROM

VEHICLES

(See 6.5)

1.0 GENERAL


configuration "REESS charging mode coupled to the power grid".

1.2 Test method

This test is intended to measure the level of radio frequency conducted

disturbances generated by vehicle in configuration "REESS charging mode

coupled to the power grid" through its AC or DC power lines in order to ensure

it is compatible with residential, commercial and light industrial environments.


CISPR 16-2-1.



power grid".





starting the next sub-bands). If the current consumption can be adjusted, then

the current shall be set to at least 80 per cent of its nominal value.




3.0 Test arrangements

3.1 The test shall be performed according to paragraph 6.4.1. of CISPR 16-2-1 as

floor-standing equipment.

3.2 The artificial mains network to be used for the measurement on vehicle is

defined in paragraph 4.3. of CISPR 16-1-2.

106/149

Artificial networks

AIS

-004 (P

art 3

) (Rev

.1)

The AN(s) shall be mounted directly on the ground plane. The cases of the AN(s) shall be bonded to the ground plane.

The measuring port of each AN shall be terminated with a 50ohm load.

The AN shall be placed as defined in Figures 1a to 1d. of Appendix 1 to this annex.

3.3 The test set-up for the connection of the vehicle in configuration "REESS charging mode coupled to the power grid" is shown in

Figure 1a to 1d of Appendix 1 to this annex.


Table 1 and 2.

Table 1

Spectrum analyzer parameters

Frequency

Range, MHz

Peak Detector Quasi-peak detector Average Detector

RBW at -3dB Scan Time RBW at -6dB Scan Time RBW at -3dB Scan Time

0.15 to 30 9/10 kHz 10 s/MHz 9 kHz 200 s/MHz 9/10 kHz 10 s/MHz

Note: If a spectrum analyzer is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth

(RBW)

Table 2


Frequency

range,

MHz

Peak Detector Quasi-peak detector Average Detector


time

BW at -6 dB Step

size(a)

Dwell

time


time

0.15 to 30 9 kHz 5 kHz 50 ms 9 kHz 5 kHz 1 s 9 kHz 5 kHz 50 ms

(a) For purely broadband disturbances, the maximum frequency step size may be increased up to a value not greater than the bandwidth

value.


107/149


4.1 The limits apply throughout the frequency range 0.15 to 30 MHz for


4.2 Measurements shall be performed with average and either quasi-peak or peak

detectors. The limits are given in paragraph 6.5. of this Standard.

Table 7 for AC lines and Table 8 for DC lines. If peak detectors are used a

correction factor of 20 dB as defined in CISPR 12 shall be applied.


108/149


Figure 1 Vehicle in configuration "REESS charging mode coupled to the

power grid"

Example of test setup for vehicle with plug located on vehicle side (AC


Figure 1a - Front View

Figure1b – Top View

Legend:

1 Vehicle under test 4 Artificial network(s) grounded (for AC or

DC power lines)

2 Insulating support 5 Power mains socket

3 Charging cable 6 Measuring receiver


109/149

Vehicle in configuration "REESS charging mode coupled to the power grid"

Example of test setup for vehicle with plug located front / rear of vehicle (AC




Legend:

1 Vehicle under test 4 Artificial network(s) grounded (for AC

or DC power lines)




110/149

ANNEX 12

METHOD(S) OF TESTING FOR EMISSION OF RADIO FREQUENCY

CONDUCTED DISTURBANCES ON NETWORK AND

TELECOMMUNICATION ACCESS FROM VEHICLES

(See 6.6)

1.0 GENERAL

1.1 The Test method described in this annex shall be applied to vehicles in

configuration "REESS charging mode coupled to the power

1.2 Test method


disturbances generated by vehicle in configuration "REESS charging mode

coupled to the power grid" through its network and telecommunication access

in order to ensure it is compatible with residential, commercial and light

industrial environments.


CISPR 32.

2.0 VEHICLE/ STATE DURING TESTS


power grid". The state of charge (SOC) of the traction battery shall be kept

between 20 per cent and 80 per cent of the maximum SOC during the whole

frequency range measurement (this may lead to split the measurement in

different sub-bands with the need to discharge the vehicle's traction battery

before starting the next sub-bands). If the current consumption can be adjusted,






3.1 The test set-up shall be performed according to paragraph 5. of CISPR 32 for

conducted emissions.

3.2 The impedance stabilization to be used for the measurement on vehicle is

defined in paragraph C.4.1.2 of CISPR 32.

Impedance Stabilization




The measuring port of each IS shall be terminated with a 50 Ω load. The

IS shall be placed as defined in Figures 1a to 1d of Appendix 1 to this annex.

111/149

3.3 The test set-up for the connection of the vehicle in configuration "REESS charging mode coupled to the power grid" is shown in

Figures 1a to 1d of Appendix 1 to this annex.

AIS

-004 (P

art 3

) (Rev

.1)

If it is impossible to guarantee the functionality of vehicle, due to introduction of IS, an alternate method described in CISPR 32

(according to Figures 2a to 2d of Appendix 1 to this annex) shall be applied.



Table 1


Frequency

range MHz





(RBW).

Table 2


Frequency

range, MHz


BW at -6 dB Step Size (a) Dwell

Time

BW at -6 dB Step Size (a) Dwell

Time

BW at -6 dB Step Size (a) Dwell Time



value.


112/149





detectors. The limits are given in Table 9 of paragraph 7.6. If peak detectors are

used a correction factor of 20 dB as defined in CISPR 12 shall be applied.


113/149


Figure 1


grid"

Example of test setup for vehicle with plug located on vehicle side




Legend:

1 Vehicle under test 5 Power mains socket

2 Insulating support 6 Impedance stabilization(s) grounded (for

communication lines)

3 Charging / communication

cable

7 Charging station

4 AC or DC artificial

network(s) grounded (for AC

or DC power lines)

8 Measuring receiver


114/149


grid"

Example of test set-up for vehicle with plug located front/rear of vehicle




Legend:

1 Vehicle under test 5 Power mains socket

2 Insulating support 6 Impedance stabilization(s) grounded (for

communication lines)

3 Charging / communication

cable

7 Charging station

4 AC or DC artificial

network(s) grounded (for AC

or DC power lines)



115/149

Alternative measurement for vehicle in configuration "REESS charging

mode coupled in the power grid"

Example of test setup for vehicle with plug located front / rear of vehicle




Legend:

1 Vehicle under test 7 Charging station

2 Insulating support 8 Current probe (or capacitive voltage

probe)

3 Charging / communication cable 9 Communication lines

4 AC or DC artificial network(s)

grounded (for AC or DC power

lines)


5 Power mains socket 11 Capacitive voltage probe


116/149

ANNEX 13

METHOD OF TESTING FOR IMMUNITY OF VEHICLES TO ELECTRICAL

FAST TRANSIENT/BURST DISTURBANCES CONDUCTED ALONG AC AND

DC POWER LINES

(See 6.8)

1.0 GENERAL

1.1 The test method described in this annex shall only be applied to vehicles. This

method concerns only the configuration of the vehicle with "REESS charging mode

coupled to the power grid".

1.2 Test method

This test is intended to demonstrate the immunity of the vehicle electronic systems.

The vehicle shall be subject to electrical fast transient / burst disturbances conducted

along AC and DC power lines of the vehicle as described in this annex. The vehicle

shall be monitored during the tests.


IEC 61000-4-4.

2.0 VEHICLE STATE DURING TESTS IN CONFIGURATION "REESS IN

CHARGING MODE COUPLED TO THE POWER GRID"

2.1 The vehicle shall be in an unladen condition except for necessary test equipment.

2.1.1 The vehicle shall be immobilized, engine OFF and in charging mode.

2.1.2 Basic vehicle conditions

The paragraph defines minimum test conditions (as far as applicable) and failures

criteria for vehicle immunity tests. Other vehicle systems, which can affect

immunity related functions, shall be tested in a way to be agreed between


"REESS charging mode" vehicle test

conditions

Failure criteria

The REESS shall be in charging mode.

The state of charge (SOC) of the

traction battery shall be kept between

20 per cent and 80 per cent of the

maximum SOC during the whole time

duration of the measurement (this may

lead to the measurement being split into

different time slots with the need to

discharge the vehicle’s traction battery

before starting the next time slot).

If the current consumption can be

adjusted, then the current shall be set to

at least 20 per cent of its nominal value.

Vehicle sets in motion


117/149

2.1.3 All other equipment which can be switched on permanently by the driver or


2.2 Only non-perturbing equipment shall be used while monitoring the vehicle.

The vehicle exterior and the passenger compartment shall be monitored to

determine whether the requirements of this annex are met (e.g. by using (a) video

camera(s), a microphone, etc.).

3.0 TEST EQUIPMENT

3.1 The test equipment is composed of a reference ground plane (a shielded room is not

required), a transient/burst generator, Coupling/Decoupling Network (CDN) and

capacitive coupling clamp

3.2 The transient/burst generator shall meet the condition defined in paragraph 6.1. of

IEC 61000-4-4.

3.3 The Coupling/Decoupling Network shall meet the condition defined in paragraph

6.2. of IEC 61000-4-4. When the Coupling/Decoupling Network cannot be used on

AC or DC power lines, the capacitive coupling clamp defined in paragraph 6.3. of

IEC 61000-4-4 can be used.

4.0 TEST SETUP

4.1 The vehicle test setup is based on the laboratory type setup as described in

paragraph 7.2. of IEC 61000-4-4.

4.2 The vehicle shall be placed directly on the ground plane.

4.3 The Test Agency shall perform the test as specified in paragraph 6.8.2.1. of this

Standard.

Alternatively, if the manufacturer provides measurement from a test laboratory

accredited to the applicable parts of ISO 17025 and recognized by the Type

Approval Authority, the Test Agency may choose not to perform the test to confirm

that the vehicle meets the requirements of this annex.

5.0 GENERATION OF REQUIRED TEST LEVEL


5.1.1 The test method according to IEC 61000-4-4 shall be used to establish the test level

requirements.

5.1.2 Test phase

The vehicle shall be positioned on the ground plane. The electrical fast

transient/burst (EFT/B) shall be applied on the vehicle on the AC/DC power lines in

common modes by using CDN as described in Figure 1 of Appendix 1 to this annex.

The test set-up shall be noted in the test report.


118/149


Figure 1


grid coupling


119/149

ANNEX 14

METHOD OF TESTING FOR IMMUNITY OF VEHICLES TO SURGES

CONDUCTED ALONG AC AND DC POWER LINES

(See 6.9)

1.0 GENERAL

1.1 The test method described in this annex shall only be applied to vehicles. This

method concerns only the configuration of the vehicle with "REESS charging mode

coupled to the power grid".

1.2 Test method

This test is intended to demonstrate the immunity of the vehicle electronic systems.

The vehicle shall be subject to surges conducted along AC and DC power lines of

the vehicle as described in this annex. The vehicle shall be monitored during the

tests.

If not otherwise stated in this annex the test shall be performed according to I EC

61000-4-5.

2.0 VEHICLE STATE DURING TESTS IN CONFIGURATION "REESS IN

CHARGING MODE COUPLED TO THE POWER GRID"

2.1 The vehicle shall be in an unladen condition except for necessary test equipment.

2.1.1 The vehicle shall be immobilized, engine OFF and in charging mode.

2.1.2 Basic vehicle conditions


criteria for vehicle immunity tests. Other vehicle systems, which can affect

immunity related functions, shall be tested in a way to be agreed between


"REESS charging mode" vehicle test

conditions

Failure criteria

The REESS shall be in charging mode.

The state of charge (SOC)

of the traction battery shall be kept

between 20 per cent and 80 per cent of

the maximum SOC during the whole

time duration of the measurement (this

may lead to the measurement being split

into different time slots with the need to

discharge the vehicle’s traction battery

before starting the next time slot).




Vehicle sets in motion


120/149

2.1.3 All other equipment which can be switched on permanently by the driver or


2.2 Only non-perturbing equipment shall be used while monitoring the vehicle. The

vehicle exterior and the passenger compartment shall be monitored to determine

whether the requirements of this annex are met (e.g. by using (a) video

camera(s), a microphone, etc.).

3.0 TEST EQUIPMENT

3.1 The test equipment is composed of a reference ground plane (a shielded room is

not required), a surge generator and a Coupling/Decoupling Network (CDN).

3.2 The surge generator shall meet the condition defined in paragraph 6.1.

of IEC 61000-4-5.

3.3 The Coupling/Decoupling Network shall meet the condition defined in


4.0 TEST SETUP

4.1 The vehicle test setup is based on the setup described in paragraph 7.2. of IEC

61000-4-5.

4.2 The vehicle shall be placed directly on the ground plane.


Standard.



Approval Authority, the Test Agency may choose not to perform the test to

confirm that the vehicle meets the requirements of this annex.



5.1.1 The test method according to IEC 61000-4-5 shall be used to establish the test

level requirements.

5.1.2 Test phase

The vehicle shall be positioned on the ground plane. The electrical surge shall

be applied on the vehicle on the AC/DC power lines between each line and earth

and between lines by using CDN as described in Figures 1 to 4 of Appendix 1 to

this annex.

The test setup shall be noted in the test report.


121/149



grid"

Figure 1


grid" – Coupling between lines for DC or AC (single phase) power lines

Figure 2


grid" – Coupling between each line and earth for DC or AC (single phase)

power lines

Figure 3


grid" –Coupling between lines for AC (Three Phase) power lines.


122/149

Figure 4


grid" – Coupling between each line and earth for AC (three phases) power

lines


123/149

ANNEX 15

METHOD(S) OF TESTING FOR EMISSION OF HARMONICS GENERATED

ON AC POWER LINES FROM AN ESA

(See 6.11)

1.0 GENERAL

1.1 The test method described in this annex shall be applied to ESAs in configuration

"REESS charging mode coupled to the power grid"

1.2 Test method

This test is intended to measure the level of harmonics generated by an ESA in

configuration "REESS charging mode coupled to the power grid" through its

AC power lines in order to ensure it is compatible with residential, commercial

and light industrial environments.


(a) IEC 61000-3-2 for input current in charging mode ≤ 16 A per phase for class

A equipment;

(b) IEC 61000-3-12 for input current in charging mode > 16 A and ≤ 75 A

per phase.


2.1 The ESA shall be in configuration "REESS charging mode coupled to the power

grid".

The state of charge (SOC) of the traction battery shall be kept between 20 per

cent and 80 per cent of the maximum SOC during the whole time duration of the

measurement (this may lead to the measurement being split into different time

slots with the need to discharge the vehicle’s traction battery before starting the

next time slot).

If the current consumption can be adjusted, then the current shall be set to at least

80 per cent of its nominal value.


3.1 The observation time to be used for the measurements shall be as for

quasi-stationary equipment as defined in Table 4 of IEC 61000-3-2.

3.2 The test set-up for single phase ESA in configuration "REESS charging mode


3.3 The test set-up for three-phase ESA in configuration "REESS charging mode



124/149


4.1 The measurements of even and odd current harmonics shall be performed up to

the 40th harmonic.

4.2 The limits for single phase or three-phase ESAs in configuration

"REESS charging mode coupled to the power grid" with input current ≤ 16 A

per phase are given in Table 10 of paragraph 6.11.2.1. of this Standard.

4.3 The limits for single phase ESAs in configuration "REESS charging mode

coupled to the power grid" with input current > 16 A and ≤ 75 A per phase are

given in Table 11 of paragraph 6.11.2.2. of this Standard.

4.4 The limits for three-phase ESAs in configuration "REESS charging mode

coupled to the power grid" with input current > 16 A and ≤ 75 A per phase are

given in paragraph Table 12 of 6.11.2.2. of this Standard.

4.5 For three-phase ESAs in configuration "REESS charging mode coupled to the

power grid" with input current > 16 A and ≤ 75 A per phase, when at least one of

the three conditions a), b) or c) described in paragraph 5.2. of IEC 61000-3-12 is

fulfilled, then the limits given in Table 13 of paragraph 6.11.2.2. of this Standard

can be applied.


125/149


Figure 1

ESA in configuration "REESS charging mode coupled to the power grid" –

Single phase test set-up

Figure 2

ESA in configuration "REESS charging mode coupled to the power grid"

–Three-phase test set-up


126/149

ANNEX 16

(See 6.12)

METHOD(S) OF TESTING FOR EMISSION OF VOLTAGE CHANGES,

VOLTAGE FLUCTUATIONS AND FLICKER ON AC POWER LINES FROM

AN ESA

1.0 GENERAL

1.1 The test method described in this annex shall be applied to ESAs in configuration

"REESS charging mode coupled to the power grid"

1.2 Test method

This test is intended to measure the level of voltage changes, voltage fluctuations

and flicker generated by ESA in configuration "REESS charging mode coupled

to the power grid" through its AC power lines in order to ensure it is compatible

with residential, commercial and light industrial environments.


(a) IEC 61000-3-3 for rated current in "REESS charging mode" ≤ 16 A per phase

and not subjected to conditional connection;

(b) IEC 61000-3-11 for rated current in "REESS charging mode" > 16 A and ≤ 75 A

per phase and subjected to conditional connection



grid"


20 per cent and 80 per cent of the maximum SOC during the whole time duration

of the measurement (this may lead to the measurement being split into different

time slots with the need to discharge the vehicle’s traction battery before starting

the next time slot).

If the current consumption can be adjusted, then the current shall be set to at least

80 per cent of its nominal value.


3.1 The tests for ESA in configuration "REESS charging mode coupled to the power

grid" with rated current ≤ 16 A per phase and not subjected to conditional


3.2 The tests for ESA in configuration "REESS charging mode coupled to the power

grid" with rated current > 16 A and ≤ 75 A per phase and subjected to conditional



127/149

3.3 The test set-up for ESA in configuration "REESS charging mode coupled to the

power grid" is shown in Figures 1a and 1b of Appendix 1 to this annex.

4.0 Test requirements

4.1 The parameters to be determined in the time-domain are "short duration flicker

value", "long duration flicker value" and "voltage relative variation".

4.2 The limits for ESA in configuration "REESS charging mode coupled to the

power grid" with input current ≤ 16 A per phase and not subjected to conditional

connection are given in paragraph 6.12.2.1. of this Standard.

4.3 The limits for ESA in configuration "REESS charging mode coupled to the

power grid" with input current > 16 A and ≤ 75 A per phase and subjected to

conditional connection are given in paragraph 6.12.2.2. of this Standard.


128/149


Figure 1a

ESA in configuration "REESS charging mode coupled to the power grid"-

Single phase test set-up

Figure 1b

ESA in configuration "REESS charging mode coupled to the power grid" -

Three-phase test set-up


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ANNEX 17

METHOD(S) OF TESTING FOR EMISSION OF RADIOFREQUENCY

CONDUCTED DISTURBANCES ON AC OR DC POWER LINES FROM AN ESA

(See 6.13)

1.0 GENERAL

The test method described in this annex shall be applied to ESAs in


1.1 The test method described in this annex shall be applied to ESAs in


1.2 Test method


disturbances generated by ESA in configuration "REESS charging mode

coupled to the power grid" through its AC or DC power lines in order to ensure

it is compatible with residential, commercial and light industrial environments.


CISPR 16-2-1.


2.1 The ESA shall be in configuration "REESS charging mode coupled to the

power grid".










3.1 The test shall be performed according to paragraph 7.4.1. of CISPR 16-2-1 as

table-standing equipment.

3.2 The artificial mains network to be used for the measurement on vehicle

components is defined in paragraph 4.3. of CISPR 16-1-2.

Artificial networks



The conducted emissions on AC and DC power lines are measured

successively on each power line by connecting the measuring receiver on the

measuring port of the related AN, the measuring port of the AN inserted in the

other power lines being terminated with a 50 Ω load.

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The AN shall be placed in front, aligned and on the same side of the vehicle power charging plug.

AIS

-004 (P

art 3

) (Rev

.1)

3.3 The test set-up for the connection of the ESAs in configuration "REESS charging mode coupled to the power grid" is shown in

Figure 1 of Appendix 1 to this annex.



Table 1


Frequency

range

MHz





(RBW).

Table 2


Frequency

range

MHz



time


time


time



value.

Note: For emissions generated by brush commutator motors without an electronic control unit, the maximum step size may be increased

up to five times the bandwidth.


131/149

4.0 Test Requirements




detectors. The limits are given in Table 14 of paragraph 6.13.2.1. of this

Standard for AC lines and in Table 15 of paragraph 6.13.2.2. of this Standard

for DC lines. If peak detectors are used a correction factor of 20 dB as defined

in CISPR 12 shall be applied


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Figure 1


Legend:

1 ESA under test 4 AC or DC Artificial network(s) grounded




133/149

ANNEX 18

(See 6.14)

METHOD(S) OF TESTING FOR EMISSION OF RADIOFREQUENCY

CONDUCTED DISTURBANCES ON NETWORK AND

TELECOMMUNICATION ACCESS FROM AN ESA

1.0 GENERAL

1.1 The test method described in this annex shall be applied to ESAs in


1.2 Test method


disturbances generated by ESA in configuration "REESS charging mode

coupled to the power grid" through its network and telecommunication access in

order to ensure it is compatible with residential, commercial and light industrial

environments.


CISPR 32.



grid".










3.1 The test set-up shall be performed according to paragraphs 8 and 9 of CISPR 32

for conducted emissions.


Communication lines shall be applied to the ESA through the Impedance

Stabilization(s)s (IS)(s).

IS to be connected in the network and communication cables is defined in

paragraph C.4.1.2. of CISPR 32



The conducted emissions on network and telecommunication lines are

measured successively on each line by connecting the measuring receiver on the

measuring port of the related IS, the measuring port of the IS inserted in the

other lines being terminated with a 50 Ω load.

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The IS shall be placed in front, aligned and on the same side of the vehicle power charging plug.

AIS

-004 (P

art 3

) (Rev

.1)

3.3 The test set-up for the connection of the ESA in configuration "REESS charging mode coupled to the power grid" is shown in Figure 1 of

Appendix 1 to this annex.

3.4 The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and

Table 2.

Table 1


Frequency

range MHz




Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW).

Table 2


Frequency

range MHz



time


time


time




4.1 The limits apply throughout the frequency range 0.15 to 30 MHz for measurements performed in a semi anechoic chamber or an outdoor test

site.

4.2 Measurements shall be performed with average and either quasi-peak or peak detectors. The limits are given in Table 16 of paragraph

6.14.2.1. of this Standard. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied.


135/149


Figure 1


Legend:

1 ESA under test 5 Power mains socket

2 Insulating support 6 Impedance stabilization(s) grounded

3 Charging /

communication cable

7 Charging station

4 AC or DC Artificial

network(s) grounded



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ANNEX 19

(SEE 6.15)

METHOD OF TESTING FOR IMMUNITY OF AN ESA TO ELECTRICAL

FAST TRANSIENT/BURST DISTURBANCES CONDUCTED ALONG AC

AND DC POWER LINES

1.0 GENERAL

1.1 The test method described in this annex shall only be applied to ESAs. This

method applies only to ESA in configuration "REESS charging mode coupled to

the power grid".

1.2 Test method

This test is intended to demonstrate the immunity of the ESA. The ESA shall be

subject to Electrical Fast Transient/Burst disturbances conducted along AC and

DC power lines of the ESA as described in this annex. The ESA shall be monitored

during the tests.

If not otherwise stated in this annex the test shall be performed according to IEC

61000-4-4.

2.0 ESA state during tests in configuration "REESS in charging mode coupled to

the power grid"

2.1 Basic ESA conditions


criteria for ESA immunity tests.

REESS charging mode" ESA test

conditions

Failure criteria

ESA shall be in configuration "REESS

charging mode coupled to the power

grid".

The state of charge (SOC) of the traction

battery shall be kept between 20 per cent

and 80 per cent of the maximum SOC

during the whole time duration of the

measurement (this may lead to the

measurement being split into different

time slots with the need to discharge the

vehicle’s traction battery before starting

the next time slot).




Incorrect charging condition (e.g.

over-current, overvoltage)


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2.2 Only non-perturbing equipment shall be used while monitoring the ESA. The

ESA shall be monitored to determine whether the requirements of this annex

are met (e.g. by using (a) video camera(s), a microphone, etc.).

3.0 TEST EQUIPMENT


not required), a transient / burst generator, Coupling Decoupling Network

(CDN) and capacitive coupling clamp.

3.2 The transient/burst generator shall meet the condition defined in paragraph 6.1.

of IEC 61000-4-4.


paragraph 6.2. of IEC 61000-4-4. When the Coupling/Decoupling Network

cannot be used on AC or DC power lines, the capacitive coupling clamp

defined in paragraph 6.3. of IEC 61000-4-4 can be used.

4.0 TEST SET-UP

4.1 The ESA test setup is based on the laboratory type set-up as described in


4.2 The ESA shall be placed directly on the ground plane.

4.3 The Test Agency shall perform the test as specified in paragraph 6.15.2.1. of

this Standard.







5.1.1 The test method according to IEC 61000-4-4 shall be used to establish the test level

requirements.

5.1.2 Test phase

The ESA shall be positioned on the ground plane. The Electrical Fast Transient/Burst

(EFT/B) shall be applied on the ESA on the AC/DC power lines in common modes by

using CDN as described in Figure 1 of Appendix 1 to this annex.

The test setup shall be noted in the test report.


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Figure 1



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ANNEX 20

METHOD OF TESTING FOR IMMUNITY OF ESAs TO SURGES

CONDUCTED ALONG AC AND DC POWER LINES

(See 6.16)

1.0 GENERAL

1.1 The test method described in this annex shall only be applied to ESAs. This

method applies only to ESAs in configuration "REESS charging mode coupled

to the power grid".

1.2 Test method

This test is intended to demonstrate the immunity of the ESA. The ESA shall be

subject to surges conducted along AC and DC power lines of the ESA as

described in this annex. The ESA shall be monitored during the tests.


IEC 61000-4-5.

2.0 ESA state during tests in configuration "REESS in charging mode

coupled to the power grid"

2.1 The ESA shall be in charging mode

2.1.2 Basic ESA conditions


failures criteria for ESA immunity tests.

REESS charging mode" ESA test

conditions

Failure

criteria

ESA shall be in configuration

"REESS charging mode coupled to

the Power grid". The state of charge

(SOC) of the traction battery shall be

kept between 20 per cent and 80 per

cent of the maximum SOC during

the whole time duration of the

measurement (this may lead to the

measurement being split into

different sub-bands with the need to

discharge the vehicle’s traction

battery before starting the next

sub-bands). If the current

consumption can be adjusted, then

the current shall be set to at least 20

per cent of its nominal value.

Incorrect charging condition (e.g. over-

current, overvoltage)


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2.2 Only non-perturbing equipment shall be used while monitoring the ESA. The

ESA shall be monitored to determine whether the requirements of this annex are

met (e.g. by using (a) video camera(s), a microphone, etc.).

3.0 TEST EQUIPMENT


not required), a surge generator and a Coupling/Decoupling Network (CDN).

3.2 The surge generator shall meet the condition defined in paragraph 6.1. of

IEC 61000-4-5.



4.0 TEST SET-UP

4.1 The ESA test set-up is based on the set-up described in paragraph 7.2. of

IEC 61000-4-5.

4.2 The ESA shall be placed directly on the ground plane.


Standard.







5.1.1 The test method according to IEC 61000-4-5 shall be used to establish the test

level requirements.

5.1.2 Test phase

The ESA shall be positioned on the ground plane. The electrical surge shall be

applied on the ESA on the AC/DC power lines between each line and earth and

between lines by using CDN as described in Figures 1 to 4 of Appendix 1 to this

annex.

The test set-up shall be noted in the test report


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Figure 1


Coupling between lines for DC or AC (single phase) power lines

Figure 2


– Coupling between each line and earth for DC or AC (single phase) power

lines

Figure 3

ESA in configuration "REESS charging mode coupled to the power

grid" - Coupling between lines for AC (three phases) power lines


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Figure 4


Coupling between each line and earth for AC (three phases) power lines


143/149

ANNEX 21A

GUIDELINES FOR DECIDING APPLICABILITY,

WORST CASE CRITERIA (WCC) AND CRITERIA FOR

EXTENSION OF APPROVAL (CEA) FOR RADIATED IMMUNITY TEST

(See 8.2)

Applicability:

1. Vehicle fitted with any of the Electronic Sub-Assembly (ESA) as per list given

below shall be subjected to immunity test:

Sr. No.

ESA

1. Electronic Engine Control Unit (ECU) for

• Fuel injection

• Ignition timing control

• Combined fuel injection and ignition timing control

• Engine valve control

• EGR

• Idle speed control

• Exhaust emission / after-treatment control

• Air-fuel ratio control

• Electronic carburetor

2. Drive by Wire System (Electronic Accelerator Pedal and/or Electronic

Brake)

3. Cruise Control System

4. Anti-skid Braking System (ABS)

5. Electronic 4-wheel Drive

6. Electronic Gear Shift Control System (Automatic Transmission or CVT)

7. Electronic Steering Control (Electronic Power Steering)

8. Motor Control Unit in case of BOVs

9. Electronic Speed Limiter

10. Air Bag and Safety Restraint System

11. Electronic Seat Adjustment Control System


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12. Electronic Rear View, Side View Mirror Adjustment Control System

13. Electronic Lamp Control Device

14. Electronic Headlamp Leveling / Adjustment System

15. Gas-discharge Headlamp with Electronic Ballast

16. Electronic Rotating Identification Lamp and/or Siren Combination

17. Stop Lamp, Rear Position Lamp, End Outline Marker Lamp using

Electronic Components such as LED etc.

18. Electronic Flasher with Direction Indicators

19. Electronic Horn

20. Electronic Anti-Theft Device for Unauthorized Use including RF

Immobiliser and Vehicle Alarm System

21. Automatic Door Lock System including Infrared Door Lock System

22. Electronic Suspension Control

23. Electronic Instrument Cluster including on-board indicators related to

functions as specified in Cl. 2.12

24. Navigation System

25. Wiper Control System

26. Tire Pressure Monitoring System

27. Digital Tachograph

28. Telematic System

The above list is not exhaustive and it is for guidance only. Due to continuous

technological advancements, it is not practicable to list all the ESAs that will require

immunity test. In such case, guidelines for immunity related vehicle functions as per Cl.

2.12 shall be considered.

2. Any change in parameters mentioned below will require separate immunity

test as per below table:

Sr. No. Parameter Immunity Test

Needed

Remarks

1. Change in engine

location

Yes Change in position and general

mounting arrangement of

engine consequent to

situations like front engine to

rear engine etc.

2. Change in body

style and or material

affecting overall

shielding of vehicle

electronics

Yes e.g. roof top body, drive away

chassis, passenger vehicle to

goods vehicle, metallic body to

non-metallic body and vice

versa etc.


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3. Change in make,

identification

mark/part number

of ESA as a result

of change in design

of hardware or

vendor of ESA or

addition of new

ESA altogether.

Yes These changes affect

immunity performance of

ESA and hence that of the

vehicle.

Changes other than those listed above are considered to be having no adverse effect on

Immunity requirements of vehicle.

Worst Case Criteria (WCC):

Normally base vehicle model shall be subjected to immunity test. Where vehicle model

is with one or more variants then the variant with fully loaded version (variant

fitted with maximum electronic systems including optional ones) and one with fully

open body (e.g. drive away chassis as the case may be) shall be subjected to the

immunity test. Bi-fuel vehicle model (e.g. petrol/CNG, petrol/LPG) with petrol mode as

limp-home mode shall be tested only in gaseous mode for immunity if it involves ESAs

as above. Bi-fuel vehicle model with no limp-home mode shall be tested separately in

each fuel mode for immunity if it involves ESAs as above. However, if petrol mode of

such vehicle model is tested and type approved for immunity requirements as per this

standard earlier, then it shall not be retested in petrol mode again.

Criteria for Extension of Approval (CEA):

In the whole vehicle testing, ESAs that are fitted to the vehicle gain approval as a

separate technical unit specific to that vehicle type. For any change in ESA or addition

of new ESA in the vehicle, immunity test can be performed either on ESA as a

component or as fitted to the vehicle. ESAs can be tested and approved for immunity

requirements as a component and extension of type approval can be granted to vehicle

based on component approval when such ESAs are incorporated in the vehicle. ESAs

approved as component can be fitted in any vehicle type.


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ANNEX 21B

GUIDELINES FOR DECIDING APPLICABILITY, WORST CASE CRITERIA

(WCC) AND CRITERIA FOR EXTENSION OF APPROVAL (CEA) FOR

RADIATED EMISSION TEST.

(See 8.2)

1.0 This annex gives factors to be considered for the extension of type approval

certificate of one model to changes in technical specifications or its variant (s).

2.0 In general, when changes in technical specifications of vehicle do not affect the

performance adversely, and is still within the stipulated limits, the type approval

certificates can be extended. The changes in parameters that affect the

performance are listed in the table below as a guideline.

3.0 In the case of following changes, with respect to the vehicle tested, in the details

submitted as per Annex 1A, tests are necessary for establishing compliance as

follows: -

Sr. No. Parameter To be Tested / Not Tested

1 Change in Engine Power No test, required, if change in

power is within 10 %

consequent to changes in the

design of engine

2 Compression ratio (SI engines) No test required, if change in

compression ratio is within 10

%.

3 Changes in body and cowling For changes in overall external

body shape like closed body to

open body (e.g. drive away

chassis as the case may be) test

needed

4 Changes in size and shape of engine

compartment.

Test needed.

5 Location of HT Coil and consequent

change in location of HT cable & high

tension harness.

Test needed.

6 Change in body material such as metal

to non - metal & vice - versa.

Test needed.


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7 Change in the position and general

mounting arrangement of engine

consequent to situations like front

engine to rear engine vice - versa etc.

Test needed.

8 Change in radio interference control

equipment such as resistive spark

plug, resistive suppressor cap,

resistive HT cable and

shielded cap as declared in sr. no. 56

of Annex 1A and/or their makes

Test needed.

9 Addition of any electronic control unit

as defined in Cl. 3.1.3

Test needed.

10 Changes in electronic oscillator

frequency of electronic control unit(s)

as defined in 5.10.1

Test needed.

11 Addition of AC (air conditioning)

variant

Test needed.

12 Significant difference in the clear

opening to engine compartment

Test needed.

- Around wheel or

- Due to metal radiator construction

change.

13 Changes in body material affecting

RF shielding

Test needed

14 Bi-fuel vehicle model (e.g.

petrol/CNG, petrol/LPG) with /

without petrol mode as limp-home

mode

Test needed in gaseous mode

only

4. Above changes are listed for guidance only. It is not practicable to list all the

changes those affect EMI.


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ANNEX 22

(See Introduction)

COMPOSITION OF AISC PANEL ON

AUTOMOTIVE VEHICLES –REQUIREMENTS FOR

ELECTROMAGNETIC COMPATIBILITY

Convener Organization

Shri A. D. Deshpande Automotive Research Association of India (ARAI)

Members Representing

Shri Abhijit Mulay Automotive Research Association of India (ARAI)

Shri Manoj Desai Automotive Research Association of India (ARAI)

Shri Kamalesh Patil Automotive Research Association of India (ARAI)

Shri Nilesh Tagad Central Institute of Road Transport (CIRT)

Shri S. Ravishankar Ashok Leyland (SIAM)

Shri Adish Agarwal Bajaj Auto (SIAM)

Shri Feroz Ali Khan Hero Motocorp (SIAM)

Shri Vipin Sharma Honda Motorcycles and Scooters (SIAM)

Shri Gururaj Ravi Maruti Suzuki (SIAM)

Shri S. J. Dhinagar Maruti Suzuki (SIAM)

Shri K Kiran Kumar Mahindra Electric (SIAM)

Shri Nikhil Desai Mercedes Benz (SIAM)

Shri Rajendra Khile Renault Nissan (SIAM)

Shri Vijay Dinakaran Renault Nissan (SIAM)

Shri P S Gowrishankar TATA Motors Limited (SIAM)

Shri Raju M Toyota Kirloskar Motors Limited(SIAM)

Shri Venusuresh Yamaha Motors (SIAM)

Shri Sivakumar

Balakripshnan

Ather energy Pvt. Ltd.

Shri Uday Harite Automotive Component Manufacturing Association

(ACMA)

* At the time of approval of this Automotive Industry Standard


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ANNEX 23

(See Introduction)

COMMITTEE COMPOSITION*

Automotive Industry Standards Committee

Chairperson

Shri Neelkanth V.

Marathe

Officiating Director

The Automotive Research Association of India, Pune

Members Representing

Representative from Ministry of Road Transport and Highways

(Dept. of Road Transport and Highways), New Delhi

Representative from Ministry of Heavy Industries and Public Enterprises

(Department of Heavy Industry), New Delhi

Shri S. M. Ahuja Office of the Development Commissioner, MSME,

Ministry of Micro, Small and Medium Enterprises, New

Delhi

Shri Shrikant R. Marathe Former Chairman, AISC

Shri R.R. Singh Bureau of Indian Standards, New Delhi

Director Central Institute of Road Transport, Pune

Director Global Automotive Research Centre

Director International Centre for Automotive Technology, Manesar

Director Indian Institute of Petroleum, Dehra Dun

Director Vehicles Research and Development Establishment,

Ahmednagar

Director Indian Rubber Manufacturers Research Association

Representatives from Society of Indian Automobile Manufacturers

Shri R. P. Vasudevan Tractor Manufacturers Association, New Delhi

Shri Uday Harite Automotive Components Manufacturers Association of

India, New Delhi

Shri K. V. Krishnamurthy Indian Construction Equipment Manufacturers Association

Member Secretary

Shri Vikram Tandon

Dy. General Manager

The Automotive Research Association of India, Pune

* At the time of approval of this Automotive Industry Standard (AIS)

AUTOMOTIVE VEHICLES - REQUIREMENTS FOR … (Part 3... · 2020. 10. 16. · Automotive Vehicles...

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